command: /home/cbarnaud/salome-cfd/Salome_CFD-SCFD_V8_5_0-Code_Saturne-5_2-univ_d54f597c/modules/CFDSTUDY_v52/libexec/code_saturne/cs_solver --param setup.xml *************************************************************** (R) Code_Saturne Version 5.2.0-patch Copyright (C) 1998-2018 EDF S.A., France revision b6e2822 build Sun 29 Jul 2018 04:50:35 AM CEST MPI version 2.1 (Open MPI 1.6.5) The Code_Saturne CFD tool is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 2 of the License, or (at your option) any later version. The Code_Saturne CFD tool is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. *************************************************************** Local case configuration: Date: Tue 22 Oct 2019 11:25:04 AM CEST System: Linux 4.18.0-80.el8.x86_64 Machine: maxwell Processor: model name : Intel(R) Xeon(R) Gold 5118 CPU @ 2.30GHz Memory: 256336 MB User: cbarnaud (cbarnaud) Directory: /home/cbarnaud/salome-cfd/workdir/Shear_Driven_Cavity_Flow/tuto01BIs/test/RESU/20191022-1125 OpenMP threads: 1 Processors/node: 24 I/O read method: standard input and output, serial access I/O write method: standard input and output, serial access External libraries for partitioning: METIS SCOTCH 6.0.4 Reading metadata from file: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 4 (Nb variables ) NSCAL = 0 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) ----------------------------------------------------------- ** VOF METHOD ---------------------------------------- IVOFMT = -1 ( -1: inactive ) ( 0: active ) ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION ---------------------------------------- ICAVIT = -1 (-1: single phase flow ) ( 0: no vap./cond. model ) ( 1: Merkle's model ) ----------------------------------------------------------- ** TIME STEPPING ------------- --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Velocity 1 0.1000E+01 Pressure 0 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** STOKES ------ -- Phase continue : ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- ------------------------------------ Variable EPSILO IDIRCL ------------------------------------ Velocity 0.1000E-07 1 Pressure 0.1000E-07 1 ------------------------------------ EPSILO = (resolution precision) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculation ) ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 400 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 0 (Checkpoint frequency ) --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) -- -- -- --- Log files NTLIST = 1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) Velocity 0 Pressure 0 CourantNb -999 FourierNb -999 total_pressure -999 Local Time Step -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted by the fluid on the boundary) ipstyp = 0 (y+ at boundary) ipsttp = 0 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 0 (Dimensionless thermal flux at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization iterations) IFLXMW = 0 (ALE mass flux computation 0: thanks to vertices 1: thanks to mesh velocity) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: time dependency: fixed mesh output: at calculation end -5: name: directory: monitoring format: time_plot options: time dependency: fixed mesh output: every 1 time steps -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at calculation end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at calculation end Reading file: mesh_input Finished reading: mesh_input Number of cells: 2500 ---------------------------------------------------------- Number of cells + halo cells: 2500 ---------------------------------------------------------- Number of interior faces: 4900 ---------------------------------------------------------- Number of boundary faces: 5200 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 1 : [ 2 ; 3 [ = 4 2 : [ 3 ; 4 ] = 2496 ---------------------------------------------------------- Renumbering mesh: renumbering for cells: pre-numbering: no renumbering cells adjacent to ghost cells last: no numbering: no renumbering renumbering for interior faces: cell adjacency pre-ordering: lowest id first faces adjacent to ghost cells last: no numbering: multipass renumbering for boundary faces: numbering: no shared cell across threads Numbering for cells: type: default number of halo-adjacent elements: 2500 Numbering for interior faces: type: default number of halo-adjacent elements: 4900 Numbering for boundary faces: type: default number of halo-adjacent elements: 5200 ---------------------------------------------------------- Matrix bandwidth for volume mesh : 50 Matrix profile/lines for volume mesh : 50 Mesh coordinates: minimum and maximum X : 0.0000000e+00 1.0000000e+00 Y : 0.0000000e+00 1.0000000e+00 Z : 0.0000000e+00 1.0000000e-02 Mesh Number of cells: 2500 Number of interior faces: 4900 Number of boundary faces: 5200 Number of vertices: 5202 Groups: "Sliding_wall" boundary faces: 50 "Stationnary_walls" boundary faces: 5050 "Symmetry_plane" boundary faces: 100 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 0 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Computing geometric quantities (0.00331 s) Probe set: "probes": maximum distance between cell centers and requested coordinates: 6.260e-02 ALMAX = 0.21544E+00 (Characteristic length ) ALMAX is the cubic root of the domain volume. ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- Velocity 0.1000E+00 0.1000E+00 Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 --------------------------------- dt 0.1000E+00 0.1000E+00 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E+00 TIME STEP NUMBER 1 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1000E+01 0.1000E+01 molecular_viscos 0.1000E-02 0.1000E-02 ----------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 0 Smooth wall 5 5100 Rough wall 6 0 Symmetry 4 100 Free outlet 3 0 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.00000E+00 0.30000E+00 Friction velocity uk : 0.00000E+00 0.30000E+00 Dimensionless distance yplus : 0.00000E+00 0.30000E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.20248E-02 1858 0.90573E-08 0.35530E-02 0.59056E+01 c Velocity[X] 0.35530E-02 c Velocity[Y] 0.35297E-35 c Velocity[Z] 0.43731E-35 c Pressure 0.18679E-18 0 0.10000E+01 -0.18679E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.095343 0.14188 0.10076 0.10076 v Velocity[Y] -1.3152e-18 1.4121e-18 8.2586e-22 8.2586e-22 v Velocity[Z] -8.5014e-19 1.3218e-18 6.5036e-22 6.5036e-22 v ǁVelocityǁ 0.095343 0.14188 0.10076 0.10076 v Pressure 0 0 0 0 v CourantNb 0 0 0 0 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.200000000E+00 TIME STEP NUMBER 2 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28159E-12 0.29294E+00 Friction velocity uk : 0.28159E-12 0.29294E+00 Dimensionless distance yplus : 0.14079E-09 0.29294E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.20514E-02 1850 0.91052E-08 0.30866E-02 0.54402E+01 c Velocity[X] 0.30866E-02 c Velocity[Y] 0.27044E-35 c Velocity[Z] 0.30210E-36 c Pressure 0.17939E-18 0 0.10000E+01 -0.17939E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.091005 0.18088 0.10148 0.10148 v Velocity[Y] -2.2897e-18 2.4947e-18 2.3983e-21 2.3983e-21 v Velocity[Z] -8.4042e-19 1.3978e-18 1.2105e-21 1.2105e-21 v ǁVelocityǁ 0.091005 0.18088 0.10148 0.10148 v Pressure 0 0 0 0 v CourantNb 0 8.1629e-17 9.6287e-18 9.6287e-18 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.300000000E+00 TIME STEP NUMBER 3 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37836E-12 0.28620E+00 Friction velocity uk : 0.37836E-12 0.28620E+00 Dimensionless distance yplus : 0.18918E-09 0.28620E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.20824E-02 1843 0.90722E-08 0.26879E-02 0.50089E+01 c Velocity[X] 0.26879E-02 c Velocity[Y] 0.22652E-35 c Velocity[Z] 0.76380E-37 c Pressure 0.18454E-18 0 0.10000E+01 -0.18454E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.086964 0.21722 0.10217 0.10217 v Velocity[Y] -3.0723e-18 3.4094e-18 4.6445e-21 4.6445e-21 v Velocity[Z] -8.8427e-19 1.4955e-18 1.3576e-21 1.3576e-21 v ǁVelocityǁ 0.086964 0.21722 0.10217 0.10217 v Pressure 0 0 0 0 v CourantNb 0 8.6193e-17 9.8606e-18 9.8606e-18 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.400000000E+00 TIME STEP NUMBER 4 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75155E-12 0.27978E+00 Friction velocity uk : 0.75155E-12 0.27978E+00 Dimensionless distance yplus : 0.37577E-09 0.27978E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.21164E-02 1836 0.90407E-08 0.23467E-02 0.46123E+01 c Velocity[X] 0.23467E-02 c Velocity[Y] 0.19381E-35 c Velocity[Z] 0.39947E-37 c Pressure 0.18681E-18 0 0.10000E+01 -0.18681E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.083196 0.25109 0.10284 0.10284 v Velocity[Y] -3.728e-18 4.2226e-18 7.496e-21 7.496e-21 v Velocity[Z] -8.8859e-19 1.5108e-18 1.3023e-21 1.3023e-21 v ǁVelocityǁ 0.083196 0.25109 0.10284 0.10284 v Pressure 0 0 0 0 v CourantNb 0 9.0839e-17 1.0414e-17 1.0414e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.500000000E+00 TIME STEP NUMBER 5 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80391E-12 0.27366E+00 Friction velocity uk : 0.80391E-12 0.27366E+00 Dimensionless distance yplus : 0.40195E-09 0.27366E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.21525E-02 1829 0.90155E-08 0.20542E-02 0.42500E+01 c Velocity[X] 0.20542E-02 c Velocity[Y] 0.16729E-35 c Velocity[Z] 0.32009E-37 c Pressure 0.18993E-18 0 0.10000E+01 -0.18993E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.079681 0.2827 0.10347 0.10347 v Velocity[Y] -4.2928e-18 4.9687e-18 1.0889e-20 1.0889e-20 v Velocity[Z] -1.0064e-18 1.5229e-18 9.9687e-22 9.9687e-22 v ǁVelocityǁ 0.079681 0.2827 0.10347 0.10347 v Pressure 0 0 0 0 v CourantNb 0 9.1668e-17 1.0655e-17 1.0655e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.600000000E+00 TIME STEP NUMBER 6 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69146E-12 0.26782E+00 Friction velocity uk : 0.69146E-12 0.26782E+00 Dimensionless distance yplus : 0.34573E-09 0.26782E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.21898E-02 1821 0.90751E-08 0.18031E-02 0.39202E+01 c Velocity[X] 0.18031E-02 c Velocity[Y] 0.14562E-35 c Velocity[Z] 0.30506E-37 c Pressure 0.19298E-18 0 0.10000E+01 -0.19298E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.076399 0.3122 0.10408 0.10408 v Velocity[Y] -4.7897e-18 5.6677e-18 1.4769e-20 1.4769e-20 v Velocity[Z] -1.1314e-18 1.5241e-18 8.8251e-22 8.8251e-22 v ǁVelocityǁ 0.076399 0.3122 0.10408 0.10408 v Pressure 0 0 0 0 v CourantNb 0 9.2263e-17 1.0867e-17 1.0867e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.700000000E+00 TIME STEP NUMBER 7 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12190E-11 0.26226E+00 Friction velocity uk : 0.12190E-11 0.26226E+00 Dimensionless distance yplus : 0.60951E-09 0.26226E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.22278E-02 1815 0.89963E-08 0.15872E-02 0.36209E+01 c Velocity[X] 0.15872E-02 c Velocity[Y] 0.12612E-35 c Velocity[Z] 0.27444E-37 c Pressure 0.19622E-18 0 0.10000E+01 -0.19622E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.073334 0.33976 0.10466 0.10466 v Velocity[Y] -5.2267e-18 6.3265e-18 1.908e-20 1.908e-20 v Velocity[Z] -1.2503e-18 1.5346e-18 8.4499e-22 8.4499e-22 v ǁVelocityǁ 0.073334 0.33976 0.10466 0.10466 v Pressure 0 0 0 0 v CourantNb 0 9.2316e-17 1.1048e-17 1.1048e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.800000000E+00 TIME STEP NUMBER 8 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13970E-11 0.25695E+00 Friction velocity uk : 0.13970E-11 0.25695E+00 Dimensionless distance yplus : 0.69848E-09 0.25695E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.22659E-02 1808 0.90064E-08 0.14012E-02 0.33499E+01 c Velocity[X] 0.14012E-02 c Velocity[Y] 0.10978E-35 c Velocity[Z] 0.22642E-37 c Pressure 0.19940E-18 0 0.10000E+01 -0.19940E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.070468 0.36552 0.10522 0.10522 v Velocity[Y] -5.6103e-18 6.9491e-18 2.3775e-20 2.3775e-20 v Velocity[Z] -1.3597e-18 1.6538e-18 7.9541e-22 7.9541e-22 v ǁVelocityǁ 0.070468 0.36552 0.10522 0.10522 v Pressure 0 0 0 0 v CourantNb 0 9.2265e-17 1.1231e-17 1.1231e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.900000000E+00 TIME STEP NUMBER 9 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10560E-11 0.25189E+00 Friction velocity uk : 0.10560E-11 0.25189E+00 Dimensionless distance yplus : 0.52801E-09 0.25189E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.23037E-02 1801 0.90314E-08 0.12408E-02 0.31047E+01 c Velocity[X] 0.12408E-02 c Velocity[Y] 0.95766E-36 c Velocity[Z] 0.20978E-37 c Pressure 0.20275E-18 0 0.10000E+01 -0.20275E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.067788 0.38961 0.10576 0.10576 v Velocity[Y] -5.9488e-18 7.5417e-18 2.8808e-20 2.8808e-20 v Velocity[Z] -1.4618e-18 1.7673e-18 7.7217e-22 7.7217e-22 v ǁVelocityǁ 0.067788 0.38961 0.10576 0.10576 v Pressure 0 0 0 0 v CourantNb 0 9.4892e-17 1.1386e-17 1.1386e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.100000000E+01 TIME STEP NUMBER 10 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74094E-12 0.24706E+00 Friction velocity uk : 0.74094E-12 0.24706E+00 Dimensionless distance yplus : 0.37047E-09 0.24706E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.23411E-02 1795 0.89970E-08 0.11021E-02 0.28830E+01 c Velocity[X] 0.11021E-02 c Velocity[Y] 0.83887E-36 c Velocity[Z] 0.19734E-37 c Pressure 0.20596E-18 0 0.10000E+01 -0.20596E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.06528 0.41216 0.10628 0.10628 v Velocity[Y] -6.2444e-18 8.1052e-18 3.4138e-20 3.4138e-20 v Velocity[Z] -1.564e-18 1.8775e-18 6.1376e-22 6.1376e-22 v ǁVelocityǁ 0.06528 0.41216 0.10628 0.10628 v Pressure 0 0 0 0 v CourantNb 0 1.0123e-16 1.1534e-17 1.1534e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.110000000E+01 TIME STEP NUMBER 11 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35030E-12 0.24245E+00 Friction velocity uk : 0.35030E-12 0.24245E+00 Dimensionless distance yplus : 0.17515E-09 0.24245E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.23777E-02 1789 0.89785E-08 0.98192E-03 0.26825E+01 c Velocity[X] 0.98192E-03 c Velocity[Y] 0.73753E-36 c Velocity[Z] 0.18081E-37 c Pressure 0.20927E-18 0 0.10000E+01 -0.20927E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.062931 0.43328 0.10678 0.10678 v Velocity[Y] -6.5018e-18 8.642e-18 3.9728e-20 3.9728e-20 v Velocity[Z] -1.6666e-18 1.989e-18 4.7398e-22 4.7398e-22 v ǁVelocityǁ 0.062931 0.43328 0.10678 0.10678 v Pressure 0 0 0 0 v CourantNb 0 1.0741e-16 1.1682e-17 1.1682e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.120000000E+01 TIME STEP NUMBER 12 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56021E-12 0.23806E+00 Friction velocity uk : 0.56021E-12 0.23806E+00 Dimensionless distance yplus : 0.28010E-09 0.23806E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.24135E-02 1783 0.89758E-08 0.87766E-03 0.25011E+01 c Velocity[X] 0.87766E-03 c Velocity[Y] 0.64393E-36 c Velocity[Z] 0.17315E-37 c Pressure 0.21254E-18 0 0.10000E+01 -0.21254E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.060729 0.45307 0.10726 0.10726 v Velocity[Y] -6.7233e-18 9.1529e-18 4.5542e-20 4.5542e-20 v Velocity[Z] -1.7591e-18 2.0858e-18 6.6603e-22 6.6603e-22 v ǁVelocityǁ 0.060729 0.45307 0.10726 0.10726 v Pressure 0 0 0 0 v CourantNb 0 1.1349e-16 1.1824e-17 1.1824e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.130000000E+01 TIME STEP NUMBER 13 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78836E-12 0.23386E+00 Friction velocity uk : 0.78836E-12 0.23386E+00 Dimensionless distance yplus : 0.39418E-09 0.23386E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.24484E-02 1777 0.89886E-08 0.78700E-03 0.23369E+01 c Velocity[X] 0.78700E-03 c Velocity[Y] 0.56651E-36 c Velocity[Z] 0.12650E-37 c Pressure 0.21573E-18 0 0.10000E+01 -0.21573E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.058664 0.47164 0.10772 0.10772 v Velocity[Y] -6.9096e-18 9.6366e-18 5.1546e-20 5.1546e-20 v Velocity[Z] -1.8462e-18 2.1694e-18 3.0166e-22 3.0166e-22 v ǁVelocityǁ 0.058664 0.47164 0.10772 0.10772 v Pressure 0 0 0 0 v CourantNb 0 1.1898e-16 1.1961e-17 1.1961e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.140000000E+01 TIME STEP NUMBER 14 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90986E-12 0.22986E+00 Friction velocity uk : 0.90986E-12 0.22986E+00 Dimensionless distance yplus : 0.45493E-09 0.22986E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.24822E-02 1772 0.89425E-08 0.70798E-03 0.21882E+01 c Velocity[X] 0.70798E-03 c Velocity[Y] 0.50248E-36 c Velocity[Z] 0.15560E-37 c Pressure 0.21899E-18 0 0.10000E+01 -0.21899E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.056726 0.48906 0.10817 0.10817 v Velocity[Y] -7.0704e-18 1.0102e-17 5.7711e-20 5.7711e-20 v Velocity[Z] -1.926e-18 2.2708e-18 3.7261e-22 3.7261e-22 v ǁVelocityǁ 0.056726 0.48906 0.10817 0.10817 v Pressure 0 0 0 0 v CourantNb 0 1.2463e-16 1.2089e-17 1.2089e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.150000000E+01 TIME STEP NUMBER 15 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10169E-11 0.22604E+00 Friction velocity uk : 0.10169E-11 0.22604E+00 Dimensionless distance yplus : 0.50846E-09 0.22604E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.25151E-02 1766 0.89851E-08 0.63897E-03 0.20533E+01 c Velocity[X] 0.63897E-03 c Velocity[Y] 0.44991E-36 c Velocity[Z] 0.12844E-37 c Pressure 0.22215E-18 0 0.10000E+01 -0.22215E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.054905 0.50542 0.10861 0.10861 v Velocity[Y] -7.2038e-18 1.0544e-17 6.4014e-20 6.4014e-20 v Velocity[Z] -2.0101e-18 2.3667e-18 3.1732e-22 3.1732e-22 v ǁVelocityǁ 0.054905 0.50542 0.10861 0.10861 v Pressure 0 0 0 0 v CourantNb 0 1.2965e-16 1.2216e-17 1.2216e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.160000000E+01 TIME STEP NUMBER 16 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95042E-12 0.22239E+00 Friction velocity uk : 0.95042E-12 0.22239E+00 Dimensionless distance yplus : 0.47521E-09 0.22239E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.25469E-02 1761 0.89680E-08 0.57856E-03 0.19309E+01 c Velocity[X] 0.57856E-03 c Velocity[Y] 0.39312E-36 c Velocity[Z] 0.85578E-38 c Pressure 0.22513E-18 0 0.10000E+01 -0.22513E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.053194 0.5208 0.10903 0.10903 v Velocity[Y] -7.3088e-18 1.0962e-17 7.0426e-20 7.0426e-20 v Velocity[Z] -2.0764e-18 2.4299e-18 1.3913e-22 1.3913e-22 v ǁVelocityǁ 0.053194 0.5208 0.10903 0.10903 v Pressure 0 0 0 0 v CourantNb 0 1.3469e-16 1.2341e-17 1.2341e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.170000000E+01 TIME STEP NUMBER 17 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99436E-12 0.21891E+00 Friction velocity uk : 0.99436E-12 0.21891E+00 Dimensionless distance yplus : 0.49718E-09 0.21891E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.25776E-02 1756 0.89646E-08 0.52555E-03 0.18195E+01 c Velocity[X] 0.52555E-03 c Velocity[Y] 0.36051E-36 c Velocity[Z] 0.14959E-37 c Pressure 0.22839E-18 0 0.10000E+01 -0.22839E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.051584 0.53527 0.10944 0.10944 v Velocity[Y] -7.3972e-18 1.1368e-17 7.6928e-20 7.6928e-20 v Velocity[Z] -2.1521e-18 2.5288e-18 2.2801e-22 2.2801e-22 v ǁVelocityǁ 0.051584 0.53527 0.10944 0.10944 v Pressure 0 0 0 0 v CourantNb 0 1.3926e-16 1.2444e-17 1.2444e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.180000000E+01 TIME STEP NUMBER 18 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10195E-11 0.21558E+00 Friction velocity uk : 0.10195E-11 0.21558E+00 Dimensionless distance yplus : 0.50973E-09 0.21558E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.26073E-02 1751 0.89743E-08 0.47892E-03 0.17181E+01 c Velocity[X] 0.47892E-03 c Velocity[Y] 0.31892E-36 c Velocity[Z] 0.98786E-38 c Pressure 0.23139E-18 0 0.10000E+01 -0.23139E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.050068 0.54889 0.10984 0.10984 v Velocity[Y] -7.4627e-18 1.1752e-17 8.3497e-20 8.3497e-20 v Velocity[Z] -2.2173e-18 2.598e-18 7.7736e-23 7.7736e-23 v ǁVelocityǁ 0.050068 0.54889 0.10984 0.10984 v Pressure 0 0 0 0 v CourantNb 0 1.4388e-16 1.2574e-17 1.2574e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.190000000E+01 TIME STEP NUMBER 19 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80318E-12 0.21239E+00 Friction velocity uk : 0.80318E-12 0.21239E+00 Dimensionless distance yplus : 0.40159E-09 0.21239E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.26360E-02 1747 0.89230E-08 0.43781E-03 0.16257E+01 c Velocity[X] 0.43781E-03 c Velocity[Y] 0.28732E-36 c Velocity[Z] 0.91343E-38 c Pressure 0.23434E-18 0 0.10000E+01 -0.23434E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.04864 0.56172 0.11022 0.11022 v Velocity[Y] -7.5082e-18 1.2118e-17 9.0114e-20 9.0114e-20 v Velocity[Z] -2.2746e-18 2.6983e-18 1.5352e-22 1.5352e-22 v ǁVelocityǁ 0.04864 0.56172 0.11022 0.11022 v Pressure 0 0 0 0 v CourantNb 0 1.4856e-16 1.2681e-17 1.2681e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.200000000E+01 TIME STEP NUMBER 20 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45811E-12 0.20935E+00 Friction velocity uk : 0.45811E-12 0.20935E+00 Dimensionless distance yplus : 0.22906E-09 0.20935E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.26637E-02 1742 0.89571E-08 0.40146E-03 0.15413E+01 c Velocity[X] 0.40146E-03 c Velocity[Y] 0.26002E-36 c Velocity[Z] 0.89221E-38 c Pressure 0.23716E-18 0 0.10000E+01 -0.23716E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.047294 0.57382 0.11059 0.11059 v Velocity[Y] -7.537e-18 1.2468e-17 9.6763e-20 9.6763e-20 v Velocity[Z] -2.3471e-18 2.7373e-18 1.0879e-22 1.0879e-22 v ǁVelocityǁ 0.047294 0.57382 0.11059 0.11059 v Pressure 0 0 0 0 v CourantNb 0 1.5283e-16 1.2786e-17 1.2786e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.210000000E+01 TIME STEP NUMBER 21 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41887E-12 0.20644E+00 Friction velocity uk : 0.41887E-12 0.20644E+00 Dimensionless distance yplus : 0.20943E-09 0.20644E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.26905E-02 1738 0.89292E-08 0.36926E-03 0.14641E+01 c Velocity[X] 0.36926E-03 c Velocity[Y] 0.24286E-36 c Velocity[Z] 0.84398E-38 c Pressure 0.24014E-18 0 0.10000E+01 -0.24014E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.046024 0.58523 0.11096 0.11096 v Velocity[Y] -7.5549e-18 1.2805e-17 1.0343e-19 1.0343e-19 v Velocity[Z] -2.3964e-18 2.8438e-18 2.4057e-22 2.4057e-22 v ǁVelocityǁ 0.046024 0.58523 0.11096 0.11096 v Pressure 0 0 0 0 v CourantNb 0 1.5715e-16 1.2896e-17 1.2896e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.220000000E+01 TIME STEP NUMBER 22 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67548E-12 0.20366E+00 Friction velocity uk : 0.67548E-12 0.20366E+00 Dimensionless distance yplus : 0.33774E-09 0.20366E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.27164E-02 1734 0.89121E-08 0.34064E-03 0.13933E+01 c Velocity[X] 0.34064E-03 c Velocity[Y] 0.21266E-36 c Velocity[Z] 0.64406E-38 c Pressure 0.24282E-18 0 0.10000E+01 -0.24282E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.044824 0.59601 0.11131 0.11131 v Velocity[Y] -7.5514e-18 1.312e-17 1.101e-19 1.101e-19 v Velocity[Z] -2.4571e-18 2.8745e-18 -1.8153e-23 -1.8153e-23 v ǁVelocityǁ 0.044824 0.59601 0.11131 0.11131 v Pressure 0 0 0 0 v CourantNb 0 1.6076e-16 1.2992e-17 1.2992e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.230000000E+01 TIME STEP NUMBER 23 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57249E-12 0.20099E+00 Friction velocity uk : 0.57249E-12 0.20099E+00 Dimensionless distance yplus : 0.28624E-09 0.20099E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.27414E-02 1730 0.89053E-08 0.31515E-03 0.13284E+01 c Velocity[X] 0.31515E-03 c Velocity[Y] 0.19546E-36 c Velocity[Z] 0.62825E-38 c Pressure 0.24561E-18 0 0.10000E+01 -0.24561E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.04369 0.6062 0.11166 0.11166 v Velocity[Y] -7.5359e-18 1.3422e-17 1.1676e-19 1.1676e-19 v Velocity[Z] -2.5189e-18 2.9374e-18 -4.0348e-22 -4.0348e-22 v ǁVelocityǁ 0.04369 0.6062 0.11166 0.11166 v Pressure 0 0 0 0 v CourantNb 0 1.6472e-16 1.3076e-17 1.3076e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.240000000E+01 TIME STEP NUMBER 24 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52863E-12 0.19844E+00 Friction velocity uk : 0.52863E-12 0.19844E+00 Dimensionless distance yplus : 0.26431E-09 0.19844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.27655E-02 1726 0.89082E-08 0.29238E-03 0.12687E+01 c Velocity[X] 0.29238E-03 c Velocity[Y] 0.18097E-36 c Velocity[Z] 0.64471E-38 c Pressure 0.24825E-18 0 0.10000E+01 -0.24825E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.042618 0.61583 0.112 0.112 v Velocity[Y] -7.5107e-18 1.3712e-17 1.234e-19 1.234e-19 v Velocity[Z] -2.5617e-18 2.9923e-18 -2.0287e-22 -2.0287e-22 v ǁVelocityǁ 0.042618 0.61583 0.112 0.112 v Pressure 0 0 0 0 v CourantNb 0 1.6845e-16 1.317e-17 1.317e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.250000000E+01 TIME STEP NUMBER 25 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32079E-12 0.19600E+00 Friction velocity uk : 0.32079E-12 0.19600E+00 Dimensionless distance yplus : 0.16040E-09 0.19600E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.27889E-02 1722 0.89202E-08 0.27199E-03 0.12138E+01 c Velocity[X] 0.27199E-03 c Velocity[Y] 0.16622E-36 c Velocity[Z] 0.76484E-38 c Pressure 0.25093E-18 0 0.10000E+01 -0.25093E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.041603 0.62495 0.11233 0.11233 v Velocity[Y] -7.4768e-18 1.399e-17 1.3001e-19 1.3001e-19 v Velocity[Z] -2.6172e-18 3.0776e-18 -6.9722e-23 -6.9722e-23 v ǁVelocityǁ 0.041603 0.62495 0.11233 0.11233 v Pressure 0 0 0 0 v CourantNb 0 1.7213e-16 1.3265e-17 1.3265e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.260000000E+01 TIME STEP NUMBER 26 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70028E-12 0.19366E+00 Friction velocity uk : 0.70028E-12 0.19366E+00 Dimensionless distance yplus : 0.35014E-09 0.19366E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.28115E-02 1718 0.89410E-08 0.25368E-03 0.11631E+01 c Velocity[X] 0.25368E-03 c Velocity[Y] 0.15594E-36 c Velocity[Z] 0.64655E-38 c Pressure 0.25365E-18 0 0.10000E+01 -0.25365E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.040641 0.63359 0.11265 0.11265 v Velocity[Y] -7.4358e-18 1.4256e-17 1.3657e-19 1.3657e-19 v Velocity[Z] -2.6504e-18 3.1421e-18 2.4831e-23 2.4831e-23 v ǁVelocityǁ 0.040641 0.63359 0.11265 0.11265 v Pressure 0 0 0 0 v CourantNb 0 1.752e-16 1.3353e-17 1.3353e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.270000000E+01 TIME STEP NUMBER 27 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65011E-12 0.19142E+00 Friction velocity uk : 0.65011E-12 0.19142E+00 Dimensionless distance yplus : 0.32506E-09 0.19142E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.28334E-02 1715 0.88972E-08 0.23719E-03 0.11162E+01 c Velocity[X] 0.23719E-03 c Velocity[Y] 0.14356E-36 c Velocity[Z] 0.52153E-38 c Pressure 0.25621E-18 0 0.10000E+01 -0.25621E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.039729 0.64178 0.11296 0.11296 v Velocity[Y] -7.3847e-18 1.4509e-17 1.4309e-19 1.4309e-19 v Velocity[Z] -2.6895e-18 3.2199e-18 6.725e-23 6.725e-23 v ǁVelocityǁ 0.039729 0.64178 0.11296 0.11296 v Pressure 0 0 0 0 v CourantNb 0 1.7812e-16 1.3449e-17 1.3449e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.280000000E+01 TIME STEP NUMBER 28 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45873E-12 0.18927E+00 Friction velocity uk : 0.45873E-12 0.18927E+00 Dimensionless distance yplus : 0.22936E-09 0.18927E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.28546E-02 1711 0.89340E-08 0.22231E-03 0.10728E+01 c Velocity[X] 0.22231E-03 c Velocity[Y] 0.13353E-36 c Velocity[Z] 0.58633E-38 c Pressure 0.25876E-18 0 0.10000E+01 -0.25876E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.038864 0.64955 0.11327 0.11327 v Velocity[Y] -7.3256e-18 1.4751e-17 1.4956e-19 1.4956e-19 v Velocity[Z] -2.7396e-18 3.2681e-18 1.4216e-22 1.4216e-22 v ǁVelocityǁ 0.038864 0.64955 0.11327 0.11327 v Pressure 0 0 0 0 v CourantNb 0 1.8126e-16 1.3524e-17 1.3524e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.290000000E+01 TIME STEP NUMBER 29 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77550E-12 0.18720E+00 Friction velocity uk : 0.77550E-12 0.18720E+00 Dimensionless distance yplus : 0.38775E-09 0.18720E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.28751E-02 1708 0.89055E-08 0.20884E-03 0.10325E+01 c Velocity[X] 0.20884E-03 c Velocity[Y] 0.12463E-36 c Velocity[Z] 0.43805E-38 c Pressure 0.26115E-18 0 0.10000E+01 -0.26115E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.038043 0.65693 0.11357 0.11357 v Velocity[Y] -7.2606e-18 1.4982e-17 1.5596e-19 1.5596e-19 v Velocity[Z] -2.7919e-18 3.3093e-18 1.0098e-22 1.0098e-22 v ǁVelocityǁ 0.038043 0.65693 0.11357 0.11357 v Pressure 0 0 0 0 v CourantNb 0 1.8458e-16 1.3614e-17 1.3614e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.300000000E+01 TIME STEP NUMBER 30 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97994E-12 0.18522E+00 Friction velocity uk : 0.97994E-12 0.18522E+00 Dimensionless distance yplus : 0.48997E-09 0.18522E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.28950E-02 1705 0.88842E-08 0.19661E-03 0.99512E+00 c Velocity[X] 0.19661E-03 c Velocity[Y] 0.11655E-36 c Velocity[Z] 0.40521E-38 c Pressure 0.26348E-18 0 0.10000E+01 -0.26348E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.037262 0.66395 0.11386 0.11386 v Velocity[Y] -7.1871e-18 1.5201e-17 1.6229e-19 1.6229e-19 v Velocity[Z] -2.827e-18 3.3696e-18 -1.6259e-22 -1.6259e-22 v ǁVelocityǁ 0.037262 0.66395 0.11386 0.11386 v Pressure 0 0 0 0 v CourantNb 0 1.875e-16 1.3688e-17 1.3688e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.310000000E+01 TIME STEP NUMBER 31 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85404E-12 0.18332E+00 Friction velocity uk : 0.85404E-12 0.18332E+00 Dimensionless distance yplus : 0.42702E-09 0.18332E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29143E-02 1701 0.89421E-08 0.18549E-03 0.96029E+00 c Velocity[X] 0.18549E-03 c Velocity[Y] 0.10942E-36 c Velocity[Z] 0.40586E-38 c Pressure 0.26587E-18 0 0.10000E+01 -0.26587E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.036519 0.67062 0.11415 0.11415 v Velocity[Y] -7.1094e-18 1.5411e-17 1.6854e-19 1.6854e-19 v Velocity[Z] -2.859e-18 3.4082e-18 -6.471e-23 -6.471e-23 v ǁVelocityǁ 0.036519 0.67062 0.11415 0.11415 v Pressure 0 0 0 0 v CourantNb 0 1.9026e-16 1.3762e-17 1.3762e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.320000000E+01 TIME STEP NUMBER 32 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86838E-12 0.18149E+00 Friction velocity uk : 0.86838E-12 0.18149E+00 Dimensionless distance yplus : 0.43419E-09 0.18149E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29330E-02 1698 0.89337E-08 0.17535E-03 0.92780E+00 c Velocity[X] 0.17535E-03 c Velocity[Y] 0.10269E-36 c Velocity[Z] 0.31269E-38 c Pressure 0.26799E-18 0 0.10000E+01 -0.26799E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.035811 0.67697 0.11443 0.11443 v Velocity[Y] -7.0266e-18 1.561e-17 1.7472e-19 1.7472e-19 v Velocity[Z] -2.8866e-18 3.4593e-18 -3.5968e-22 -3.5968e-22 v ǁVelocityǁ 0.035811 0.67697 0.11443 0.11443 v Pressure 0 0 0 0 v CourantNb 0 1.9293e-16 1.3837e-17 1.3837e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.330000000E+01 TIME STEP NUMBER 33 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83194E-12 0.17973E+00 Friction velocity uk : 0.83194E-12 0.17973E+00 Dimensionless distance yplus : 0.41597E-09 0.17973E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29512E-02 1695 0.89313E-08 0.16608E-03 0.89745E+00 c Velocity[X] 0.16608E-03 c Velocity[Y] 0.96544E-37 c Velocity[Z] 0.70018E-38 c Pressure 0.27046E-18 0 0.10000E+01 -0.27046E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.035137 0.68302 0.11471 0.11471 v Velocity[Y] -6.9426e-18 1.5803e-17 1.8082e-19 1.8082e-19 v Velocity[Z] -2.9336e-18 3.5216e-18 -2.081e-22 -2.081e-22 v ǁVelocityǁ 0.035137 0.68302 0.11471 0.11471 v Pressure 0 0 0 0 v CourantNb 0 1.9531e-16 1.3898e-17 1.3898e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.340000000E+01 TIME STEP NUMBER 34 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89343E-12 0.17804E+00 Friction velocity uk : 0.89343E-12 0.17804E+00 Dimensionless distance yplus : 0.44672E-09 0.17804E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29689E-02 1692 0.89347E-08 0.15758E-03 0.86904E+00 c Velocity[X] 0.15758E-03 c Velocity[Y] 0.91482E-37 c Velocity[Z] 0.17994E-38 c Pressure 0.27251E-18 0 0.10000E+01 -0.27251E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.034495 0.68879 0.11498 0.11498 v Velocity[Y] -6.8508e-18 1.5984e-17 1.8683e-19 1.8683e-19 v Velocity[Z] -2.971e-18 3.5303e-18 -2.4487e-22 -2.4487e-22 v ǁVelocityǁ 0.034495 0.68879 0.11498 0.11498 v Pressure 0 0 0 0 v CourantNb 0 1.9859e-16 1.3991e-17 1.3991e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.350000000E+01 TIME STEP NUMBER 35 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10738E-11 0.17641E+00 Friction velocity uk : 0.10738E-11 0.17641E+00 Dimensionless distance yplus : 0.53690E-09 0.17641E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29862E-02 1689 0.89436E-08 0.14977E-03 0.84240E+00 c Velocity[X] 0.14977E-03 c Velocity[Y] 0.86287E-37 c Velocity[Z] 0.63421E-38 c Pressure 0.27476E-18 0 0.10000E+01 -0.27476E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.033882 0.6943 0.11525 0.11525 v Velocity[Y] -6.7581e-18 1.6159e-17 1.9275e-19 1.9275e-19 v Velocity[Z] -2.9971e-18 3.5976e-18 -2.5019e-22 -2.5019e-22 v ǁVelocityǁ 0.033882 0.6943 0.11525 0.11525 v Pressure 0 0 0 0 v CourantNb 0 2.0074e-16 1.404e-17 1.404e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.360000000E+01 TIME STEP NUMBER 36 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94524E-12 0.17484E+00 Friction velocity uk : 0.94524E-12 0.17484E+00 Dimensionless distance yplus : 0.47262E-09 0.17484E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30029E-02 1687 0.88852E-08 0.14258E-03 0.81739E+00 c Velocity[X] 0.14258E-03 c Velocity[Y] 0.81362E-37 c Velocity[Z] 0.43263E-38 c Pressure 0.27686E-18 0 0.10000E+01 -0.27686E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.033296 0.69955 0.11551 0.11551 v Velocity[Y] -6.6646e-18 1.6327e-17 1.9857e-19 1.9857e-19 v Velocity[Z] -3.0285e-18 3.6355e-18 -1.049e-22 -1.049e-22 v ǁVelocityǁ 0.033296 0.69955 0.11551 0.11551 v Pressure 0 0 0 0 v CourantNb 0 2.0362e-16 1.4121e-17 1.4121e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.370000000E+01 TIME STEP NUMBER 37 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11205E-11 0.17333E+00 Friction velocity uk : 0.11205E-11 0.17333E+00 Dimensionless distance yplus : 0.56026E-09 0.17333E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30193E-02 1684 0.89041E-08 0.13595E-03 0.79386E+00 c Velocity[X] 0.13595E-03 c Velocity[Y] 0.76833E-37 c Velocity[Z] 0.23032E-38 c Pressure 0.27893E-18 0 0.10000E+01 -0.27893E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.032736 0.70458 0.11577 0.11577 v Velocity[Y] -6.5627e-18 1.6481e-17 2.043e-19 2.043e-19 v Velocity[Z] -3.0592e-18 3.6814e-18 -8.1308e-23 -8.1308e-23 v ǁVelocityǁ 0.032736 0.70458 0.11577 0.11577 v Pressure 0 0 0 0 v CourantNb 0 2.0578e-16 1.4195e-17 1.4195e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.380000000E+01 TIME STEP NUMBER 38 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30250E-12 0.17188E+00 Friction velocity uk : 0.30250E-12 0.17188E+00 Dimensionless distance yplus : 0.15125E-09 0.17188E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30352E-02 1681 0.89278E-08 0.12981E-03 0.77170E+00 c Velocity[X] 0.12981E-03 c Velocity[Y] 0.73750E-37 c Velocity[Z] 0.39174E-38 c Pressure 0.28113E-18 0 0.10000E+01 -0.28113E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.032201 0.70938 0.11602 0.11602 v Velocity[Y] -6.4619e-18 1.6633e-17 2.0994e-19 2.0994e-19 v Velocity[Z] -3.1072e-18 3.7251e-18 -4.1899e-22 -4.1899e-22 v ǁVelocityǁ 0.032201 0.70938 0.11602 0.11602 v Pressure 0 0 0 0 v CourantNb 0 2.0802e-16 1.4254e-17 1.4254e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.390000000E+01 TIME STEP NUMBER 39 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34505E-12 0.17047E+00 Friction velocity uk : 0.34505E-12 0.17047E+00 Dimensionless distance yplus : 0.17252E-09 0.17047E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30507E-02 1679 0.88836E-08 0.12412E-03 0.75078E+00 c Velocity[X] 0.12412E-03 c Velocity[Y] 0.68655E-37 c Velocity[Z] 0.23436E-38 c Pressure 0.28304E-18 0 0.10000E+01 -0.28304E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.031688 0.71398 0.11627 0.11627 v Velocity[Y] -6.3595e-18 1.6774e-17 2.1547e-19 2.1547e-19 v Velocity[Z] -3.1243e-18 3.741e-18 -6.0386e-22 -6.0386e-22 v ǁVelocityǁ 0.031688 0.71398 0.11627 0.11627 v Pressure 0 0 0 0 v CourantNb 0 2.1098e-16 1.4327e-17 1.4327e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.400000000E+01 TIME STEP NUMBER 40 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73202E-12 0.16912E+00 Friction velocity uk : 0.73202E-12 0.16912E+00 Dimensionless distance yplus : 0.36601E-09 0.16912E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30658E-02 1676 0.89160E-08 0.11884E-03 0.73101E+00 c Velocity[X] 0.11884E-03 c Velocity[Y] 0.65065E-37 c Velocity[Z] 0.30933E-38 c Pressure 0.28508E-18 0 0.10000E+01 -0.28508E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.031197 0.71839 0.11652 0.11652 v Velocity[Y] -6.2589e-18 1.691e-17 2.2091e-19 2.2091e-19 v Velocity[Z] -3.1463e-18 3.7872e-18 -3.8169e-22 -3.8169e-22 v ǁVelocityǁ 0.031197 0.71839 0.11652 0.11652 v Pressure 0 0 0 0 v CourantNb 0 2.1292e-16 1.4385e-17 1.4385e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.410000000E+01 TIME STEP NUMBER 41 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E-11 0.16781E+00 Friction velocity uk : 0.10332E-11 0.16781E+00 Dimensionless distance yplus : 0.51660E-09 0.16781E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30806E-02 1674 0.88802E-08 0.11392E-03 0.71230E+00 c Velocity[X] 0.11392E-03 c Velocity[Y] 0.62434E-37 c Velocity[Z] 0.27148E-38 c Pressure 0.28703E-18 0 0.10000E+01 -0.28703E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.030726 0.72262 0.11676 0.11676 v Velocity[Y] -6.155e-18 1.7038e-17 2.2624e-19 2.2624e-19 v Velocity[Z] -3.18e-18 3.8378e-18 7.0766e-23 7.0766e-23 v ǁVelocityǁ 0.030726 0.72262 0.11676 0.11676 v Pressure 0 0 0 0 v CourantNb 0 2.1518e-16 1.4439e-17 1.4439e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.420000000E+01 TIME STEP NUMBER 42 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10865E-11 0.16655E+00 Friction velocity uk : 0.10865E-11 0.16655E+00 Dimensionless distance yplus : 0.54326E-09 0.16655E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30951E-02 1671 0.89205E-08 0.10934E-03 0.69457E+00 c Velocity[X] 0.10934E-03 c Velocity[Y] 0.58733E-37 c Velocity[Z] 0.28156E-38 c Pressure 0.28885E-18 0 0.10000E+01 -0.28885E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.030275 0.72667 0.117 0.117 v Velocity[Y] -6.0506e-18 1.716e-17 2.3147e-19 2.3147e-19 v Velocity[Z] -3.1913e-18 3.8666e-18 -6.2954e-23 -6.2954e-23 v ǁVelocityǁ 0.030275 0.72667 0.117 0.117 v Pressure 0 0 0 0 v CourantNb 0 2.1693e-16 1.4496e-17 1.4496e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.430000000E+01 TIME STEP NUMBER 43 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97099E-12 0.16533E+00 Friction velocity uk : 0.97099E-12 0.16533E+00 Dimensionless distance yplus : 0.48550E-09 0.16533E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.31092E-02 1669 0.88924E-08 0.10506E-03 0.67774E+00 c Velocity[X] 0.10506E-03 c Velocity[Y] 0.56393E-37 c Velocity[Z] 0.31225E-38 c Pressure 0.29077E-18 0 0.10000E+01 -0.29077E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.029841 0.73056 0.11724 0.11724 v Velocity[Y] -5.9441e-18 1.7275e-17 2.3661e-19 2.3661e-19 v Velocity[Z] -3.2256e-18 3.9153e-18 -1.6677e-22 -1.6677e-22 v ǁVelocityǁ 0.029841 0.73056 0.11724 0.11724 v Pressure 0 0 0 0 v CourantNb 0 2.1855e-16 1.4565e-17 1.4565e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.440000000E+01 TIME STEP NUMBER 44 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10305E-11 0.16415E+00 Friction velocity uk : 0.10305E-11 0.16415E+00 Dimensionless distance yplus : 0.51524E-09 0.16415E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.31230E-02 1666 0.89401E-08 0.10105E-03 0.66175E+00 c Velocity[X] 0.10105E-03 c Velocity[Y] 0.53987E-37 c Velocity[Z] 0.17906E-38 c Pressure 0.29251E-18 0 0.10000E+01 -0.29251E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.029424 0.7343 0.11747 0.11747 v Velocity[Y] -5.8387e-18 1.7386e-17 2.4163e-19 2.4163e-19 v Velocity[Z] -3.2441e-18 3.9331e-18 -2.4089e-22 -2.4089e-22 v ǁVelocityǁ 0.029424 0.7343 0.11747 0.11747 v Pressure 0 0 0 0 v CourantNb 0 2.2028e-16 1.4613e-17 1.4613e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.450000000E+01 TIME STEP NUMBER 45 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93940E-12 0.16300E+00 Friction velocity uk : 0.93940E-12 0.16300E+00 Dimensionless distance yplus : 0.46970E-09 0.16300E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.31366E-02 1664 0.89189E-08 0.97300E-04 0.64653E+00 c Velocity[X] 0.97300E-04 c Velocity[Y] 0.51786E-37 c Velocity[Z] 0.24167E-38 c Pressure 0.29429E-18 0 0.10000E+01 -0.29429E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.029023 0.7379 0.1177 0.1177 v Velocity[Y] -5.7308e-18 1.7489e-17 2.4656e-19 2.4656e-19 v Velocity[Z] -3.2843e-18 3.9573e-18 -4.9957e-22 -4.9957e-22 v ǁVelocityǁ 0.029023 0.7379 0.1177 0.1177 v Pressure 0 0 0 0 v CourantNb 0 2.2223e-16 1.466e-17 1.466e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.460000000E+01 TIME STEP NUMBER 46 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77080E-12 0.16190E+00 Friction velocity uk : 0.77080E-12 0.16190E+00 Dimensionless distance yplus : 0.38540E-09 0.16190E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.31498E-02 1662 0.89011E-08 0.93775E-04 0.63203E+00 c Velocity[X] 0.93775E-04 c Velocity[Y] 0.48639E-37 c Velocity[Z] 0.19649E-38 c Pressure 0.29609E-18 0 0.10000E+01 -0.29609E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.028638 0.74136 0.11792 0.11792 v Velocity[Y] -5.6255e-18 1.7587e-17 2.5138e-19 2.5138e-19 v Velocity[Z] -3.2956e-18 3.9917e-18 -6.6444e-22 -6.6444e-22 v ǁVelocityǁ 0.028638 0.74136 0.11792 0.11792 v Pressure 0 0 0 0 v CourantNb 0 2.2407e-16 1.4719e-17 1.4719e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.470000000E+01 TIME STEP NUMBER 47 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56088E-12 0.16082E+00 Friction velocity uk : 0.56088E-12 0.16082E+00 Dimensionless distance yplus : 0.28044E-09 0.16082E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.31628E-02 1660 0.88864E-08 0.90461E-04 0.61820E+00 c Velocity[X] 0.90461E-04 c Velocity[Y] 0.46738E-37 c Velocity[Z] 0.15854E-38 c Pressure 0.29776E-18 0 0.10000E+01 -0.29776E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.028266 0.74469 0.11814 0.11814 v Velocity[Y] -5.5179e-18 1.7678e-17 2.561e-19 2.561e-19 v Velocity[Z] -3.3074e-18 3.9939e-18 -8.0962e-22 -8.0962e-22 v ǁVelocityǁ 0.028266 0.74469 0.11814 0.11814 v Pressure 0 0 0 0 v CourantNb 0 2.2575e-16 1.4772e-17 1.4772e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.480000000E+01 TIME STEP NUMBER 48 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59139E-12 0.15978E+00 Friction velocity uk : 0.59139E-12 0.15978E+00 Dimensionless distance yplus : 0.29569E-09 0.15978E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.31755E-02 1657 0.89469E-08 0.87340E-04 0.60500E+00 c Velocity[X] 0.87340E-04 c Velocity[Y] 0.44853E-37 c Velocity[Z] 0.22929E-38 c Pressure 0.29944E-18 0 0.10000E+01 -0.29944E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.027908 0.7479 0.11836 0.11836 v Velocity[Y] -5.4129e-18 1.7767e-17 2.6072e-19 2.6072e-19 v Velocity[Z] -3.3212e-18 4.0271e-18 -6.6171e-22 -6.6171e-22 v ǁVelocityǁ 0.027908 0.7479 0.11836 0.11836 v Pressure 0 0 0 0 v CourantNb 0 2.2679e-16 1.4808e-17 1.4808e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.490000000E+01 TIME STEP NUMBER 49 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36786E-12 0.15878E+00 Friction velocity uk : 0.36786E-12 0.15878E+00 Dimensionless distance yplus : 0.18393E-09 0.15878E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.31880E-02 1655 0.89382E-08 0.84397E-04 0.59237E+00 c Velocity[X] 0.84397E-04 c Velocity[Y] 0.42821E-37 c Velocity[Z] 0.14165E-38 c Pressure 0.30116E-18 0 0.10000E+01 -0.30116E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.027563 0.75099 0.11858 0.11858 v Velocity[Y] -5.3046e-18 1.7846e-17 2.6523e-19 2.6523e-19 v Velocity[Z] -3.3444e-18 4.0525e-18 -1.001e-21 -1.001e-21 v ǁVelocityǁ 0.027563 0.75099 0.11858 0.11858 v Pressure 0 0 0 0 v CourantNb 0 2.293e-16 1.4867e-17 1.4867e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.500000000E+01 TIME STEP NUMBER 50 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30232E-12 0.15780E+00 Friction velocity uk : 0.30232E-12 0.15780E+00 Dimensionless distance yplus : 0.15116E-09 0.15780E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32002E-02 1653 0.89322E-08 0.81618E-04 0.58029E+00 c Velocity[X] 0.81618E-04 c Velocity[Y] 0.40098E-37 c Velocity[Z] 0.35529E-38 c Pressure 0.30296E-18 0 0.10000E+01 -0.30296E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.02723 0.75398 0.11879 0.11879 v Velocity[Y] -5.2018e-18 1.7924e-17 2.6965e-19 2.6965e-19 v Velocity[Z] -3.3654e-18 4.0962e-18 -7.6034e-22 -7.6034e-22 v ǁVelocityǁ 0.02723 0.75398 0.11879 0.11879 v Pressure 0 0 0 0 v CourantNb 0 2.3035e-16 1.4902e-17 1.4902e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.510000000E+01 TIME STEP NUMBER 51 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63493E-12 0.15685E+00 Friction velocity uk : 0.63493E-12 0.15685E+00 Dimensionless distance yplus : 0.31746E-09 0.15685E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32122E-02 1651 0.89289E-08 0.78990E-04 0.56872E+00 c Velocity[X] 0.78990E-04 c Velocity[Y] 0.38833E-37 c Velocity[Z] 0.29783E-38 c Pressure 0.30458E-18 0 0.10000E+01 -0.30458E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.026909 0.75686 0.119 0.119 v Velocity[Y] -5.1006e-18 1.8001e-17 2.7396e-19 2.7396e-19 v Velocity[Z] -3.378e-18 4.1408e-18 -6.5336e-22 -6.5336e-22 v ǁVelocityǁ 0.026909 0.75686 0.119 0.119 v Pressure 0 0 0 0 v CourantNb 0 2.3173e-16 1.4959e-17 1.4959e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.520000000E+01 TIME STEP NUMBER 52 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88724E-12 0.15593E+00 Friction velocity uk : 0.88724E-12 0.15593E+00 Dimensionless distance yplus : 0.44362E-09 0.15593E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32240E-02 1649 0.89283E-08 0.76502E-04 0.55762E+00 c Velocity[X] 0.76502E-04 c Velocity[Y] 0.37000E-37 c Velocity[Z] 0.22959E-38 c Pressure 0.30621E-18 0 0.10000E+01 -0.30621E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.026598 0.75965 0.11921 0.11921 v Velocity[Y] -5.0012e-18 1.8073e-17 2.7818e-19 2.7818e-19 v Velocity[Z] -3.4e-18 4.1267e-18 -6.7301e-22 -6.7301e-22 v ǁVelocityǁ 0.026598 0.75965 0.11921 0.11921 v Pressure 0 0 0 0 v CourantNb 0 2.3408e-16 1.5014e-17 1.5014e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.530000000E+01 TIME STEP NUMBER 53 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68860E-12 0.15503E+00 Friction velocity uk : 0.68860E-12 0.15503E+00 Dimensionless distance yplus : 0.34430E-09 0.15503E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32356E-02 1647 0.89302E-08 0.74144E-04 0.54697E+00 c Velocity[X] 0.74144E-04 c Velocity[Y] 0.35718E-37 c Velocity[Z] 0.39803E-38 c Pressure 0.30782E-18 0 0.10000E+01 -0.30782E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.026298 0.76234 0.11942 0.11942 v Velocity[Y] -4.9031e-18 1.8143e-17 2.823e-19 2.823e-19 v Velocity[Z] -3.4182e-18 4.2015e-18 -4.2006e-22 -4.2006e-22 v ǁVelocityǁ 0.026298 0.76234 0.11942 0.11942 v Pressure 0 0 0 0 v CourantNb 0 2.3469e-16 1.5056e-17 1.5056e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.540000000E+01 TIME STEP NUMBER 54 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95312E-12 0.15416E+00 Friction velocity uk : 0.95312E-12 0.15416E+00 Dimensionless distance yplus : 0.47656E-09 0.15416E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32470E-02 1645 0.89344E-08 0.71905E-04 0.53674E+00 c Velocity[X] 0.71905E-04 c Velocity[Y] 0.33728E-37 c Velocity[Z] 0.13925E-38 c Pressure 0.30940E-18 0 0.10000E+01 -0.30940E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.026007 0.76494 0.11962 0.11962 v Velocity[Y] -4.8064e-18 1.8207e-17 2.8632e-19 2.8632e-19 v Velocity[Z] -3.4301e-18 4.2226e-18 -3.5633e-22 -3.5633e-22 v ǁVelocityǁ 0.026007 0.76494 0.11962 0.11962 v Pressure 0 0 0 0 v CourantNb 0 2.3625e-16 1.5125e-17 1.5125e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.550000000E+01 TIME STEP NUMBER 55 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11353E-11 0.15332E+00 Friction velocity uk : 0.11353E-11 0.15332E+00 Dimensionless distance yplus : 0.56764E-09 0.15332E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32582E-02 1643 0.89410E-08 0.69779E-04 0.52690E+00 c Velocity[X] 0.69779E-04 c Velocity[Y] 0.31847E-37 c Velocity[Z] 0.12482E-38 c Pressure 0.31076E-18 0 0.10000E+01 -0.31076E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.025726 0.76746 0.11983 0.11983 v Velocity[Y] -4.7116e-18 1.827e-17 2.9026e-19 2.9026e-19 v Velocity[Z] -3.4451e-18 4.2348e-18 -5.563e-22 -5.563e-22 v ǁVelocityǁ 0.025726 0.76746 0.11983 0.11983 v Pressure 0 0 0 0 v CourantNb 0 2.3795e-16 1.5154e-17 1.5154e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.560000000E+01 TIME STEP NUMBER 56 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10982E-11 0.15249E+00 Friction velocity uk : 0.10982E-11 0.15249E+00 Dimensionless distance yplus : 0.54912E-09 0.15249E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32692E-02 1641 0.89499E-08 0.67756E-04 0.51743E+00 c Velocity[X] 0.67756E-04 c Velocity[Y] 0.30782E-37 c Velocity[Z] 0.10955E-38 c Pressure 0.31237E-18 0 0.10000E+01 -0.31237E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.025454 0.7699 0.12003 0.12003 v Velocity[Y] -4.6153e-18 1.8325e-17 2.941e-19 2.941e-19 v Velocity[Z] -3.4657e-18 4.2443e-18 -9.5477e-22 -9.5477e-22 v ǁVelocityǁ 0.025454 0.7699 0.12003 0.12003 v Pressure 0 0 0 0 v CourantNb 0 2.4002e-16 1.5201e-17 1.5201e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.570000000E+01 TIME STEP NUMBER 57 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11507E-11 0.15169E+00 Friction velocity uk : 0.11507E-11 0.15169E+00 Dimensionless distance yplus : 0.57535E-09 0.15169E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32800E-02 1639 0.89609E-08 0.65830E-04 0.50832E+00 c Velocity[X] 0.65830E-04 c Velocity[Y] 0.29796E-37 c Velocity[Z] 0.30767E-38 c Pressure 0.31391E-18 0 0.10000E+01 -0.31391E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.02519 0.77227 0.12022 0.12022 v Velocity[Y] -4.5232e-18 1.8381e-17 2.9786e-19 2.9786e-19 v Velocity[Z] -3.474e-18 4.2757e-18 -7.73e-22 -7.73e-22 v ǁVelocityǁ 0.02519 0.77227 0.12022 0.12022 v Pressure 0 0 0 0 v CourantNb 0 2.4088e-16 1.5239e-17 1.5239e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.580000000E+01 TIME STEP NUMBER 58 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10886E-11 0.15091E+00 Friction velocity uk : 0.10886E-11 0.15091E+00 Dimensionless distance yplus : 0.54432E-09 0.15091E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.32907E-02 1637 0.89741E-08 0.63995E-04 0.49953E+00 c Velocity[X] 0.63995E-04 c Velocity[Y] 0.28664E-37 c Velocity[Z] 0.18981E-38 c Pressure 0.31542E-18 0 0.10000E+01 -0.31542E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.024934 0.77456 0.12042 0.12042 v Velocity[Y] -4.4296e-18 1.843e-17 3.0152e-19 3.0152e-19 v Velocity[Z] -3.4929e-18 4.3138e-18 -5.0112e-22 -5.0112e-22 v ǁVelocityǁ 0.024934 0.77456 0.12042 0.12042 v Pressure 0 0 0 0 v CourantNb 0 2.4217e-16 1.5297e-17 1.5297e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.590000000E+01 TIME STEP NUMBER 59 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11116E-11 0.15015E+00 Friction velocity uk : 0.11116E-11 0.15015E+00 Dimensionless distance yplus : 0.55580E-09 0.15015E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33012E-02 1636 0.89170E-08 0.62244E-04 0.49106E+00 c Velocity[X] 0.62244E-04 c Velocity[Y] 0.27752E-37 c Velocity[Z] 0.16666E-38 c Pressure 0.31695E-18 0 0.10000E+01 -0.31695E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.024686 0.77679 0.12061 0.12061 v Velocity[Y] -4.3354e-18 1.8475e-17 3.0509e-19 3.0509e-19 v Velocity[Z] -3.5132e-18 4.3442e-18 -6.5982e-22 -6.5982e-22 v ǁVelocityǁ 0.024686 0.77679 0.12061 0.12061 v Pressure 0 0 0 0 v CourantNb 0 2.4369e-16 1.5345e-17 1.5345e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.600000000E+01 TIME STEP NUMBER 60 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13502E-11 0.14940E+00 Friction velocity uk : 0.13502E-11 0.14940E+00 Dimensionless distance yplus : 0.67512E-09 0.14940E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33116E-02 1634 0.89341E-08 0.60573E-04 0.48288E+00 c Velocity[X] 0.60573E-04 c Velocity[Y] 0.26591E-37 c Velocity[Z] 0.10926E-38 c Pressure 0.31834E-18 0 0.10000E+01 -0.31834E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.024445 0.77895 0.1208 0.1208 v Velocity[Y] -4.2431e-18 1.8516e-17 3.0857e-19 3.0857e-19 v Velocity[Z] -3.512e-18 4.3658e-18 -4.3972e-22 -4.3972e-22 v ǁVelocityǁ 0.024445 0.77895 0.1208 0.1208 v Pressure 0 0 0 0 v CourantNb 0 2.4462e-16 1.5391e-17 1.5391e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.610000000E+01 TIME STEP NUMBER 61 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13320E-11 0.14868E+00 Friction velocity uk : 0.13320E-11 0.14868E+00 Dimensionless distance yplus : 0.66600E-09 0.14868E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33218E-02 1632 0.89532E-08 0.58975E-04 0.47499E+00 c Velocity[X] 0.58975E-04 c Velocity[Y] 0.25602E-37 c Velocity[Z] 0.16438E-38 c Pressure 0.31973E-18 0 0.10000E+01 -0.31973E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.024211 0.78104 0.12099 0.12099 v Velocity[Y] -4.1503e-18 1.8553e-17 3.1196e-19 3.1196e-19 v Velocity[Z] -3.5371e-18 4.3688e-18 -9.9999e-22 -9.9999e-22 v ǁVelocityǁ 0.024211 0.78104 0.12099 0.12099 v Pressure 0 0 0 0 v CourantNb 0 2.4536e-16 1.5422e-17 1.5422e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.620000000E+01 TIME STEP NUMBER 62 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15122E-11 0.14797E+00 Friction velocity uk : 0.15122E-11 0.14797E+00 Dimensionless distance yplus : 0.75609E-09 0.14797E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33318E-02 1630 0.89741E-08 0.57447E-04 0.46735E+00 c Velocity[X] 0.57447E-04 c Velocity[Y] 0.23314E-37 c Velocity[Z] 0.20623E-38 c Pressure 0.32119E-18 0 0.10000E+01 -0.32119E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.023983 0.78308 0.12118 0.12118 v Velocity[Y] -4.0663e-18 1.8593e-17 3.1527e-19 3.1527e-19 v Velocity[Z] -3.5418e-18 4.4015e-18 -6.2754e-22 -6.2754e-22 v ǁVelocityǁ 0.023983 0.78308 0.12118 0.12118 v Pressure 0 0 0 0 v CourantNb 0 2.4689e-16 1.5455e-17 1.5455e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.630000000E+01 TIME STEP NUMBER 63 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15878E-11 0.14728E+00 Friction velocity uk : 0.15878E-11 0.14728E+00 Dimensionless distance yplus : 0.79392E-09 0.14728E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33417E-02 1629 0.89246E-08 0.55985E-04 0.45997E+00 c Velocity[X] 0.55985E-04 c Velocity[Y] 0.22580E-37 c Velocity[Z] 0.22933E-38 c Pressure 0.32255E-18 0 0.10000E+01 -0.32255E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.023762 0.78506 0.12137 0.12137 v Velocity[Y] -3.9845e-18 1.8633e-17 3.1849e-19 3.1849e-19 v Velocity[Z] -3.5602e-18 4.4119e-18 -5.3497e-22 -5.3497e-22 v ǁVelocityǁ 0.023762 0.78506 0.12137 0.12137 v Pressure 0 0 0 0 v CourantNb 0 2.4753e-16 1.5505e-17 1.5505e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.640000000E+01 TIME STEP NUMBER 64 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16021E-11 0.14661E+00 Friction velocity uk : 0.16021E-11 0.14661E+00 Dimensionless distance yplus : 0.80103E-09 0.14661E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33515E-02 1627 0.89490E-08 0.54584E-04 0.45283E+00 c Velocity[X] 0.54584E-04 c Velocity[Y] 0.22297E-37 c Velocity[Z] 0.20144E-38 c Pressure 0.32393E-18 0 0.10000E+01 -0.32393E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.023547 0.78698 0.12155 0.12155 v Velocity[Y] -3.8997e-18 1.8665e-17 3.2164e-19 3.2164e-19 v Velocity[Z] -3.5658e-18 4.4514e-18 -1.5191e-23 -1.5191e-23 v ǁVelocityǁ 0.023547 0.78698 0.12155 0.12155 v Pressure 0 0 0 0 v CourantNb 0 2.4975e-16 1.5549e-17 1.5549e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.650000000E+01 TIME STEP NUMBER 65 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14313E-11 0.14595E+00 Friction velocity uk : 0.14313E-11 0.14595E+00 Dimensionless distance yplus : 0.71563E-09 0.14595E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33611E-02 1625 0.89752E-08 0.53240E-04 0.44592E+00 c Velocity[X] 0.53240E-04 c Velocity[Y] 0.21264E-37 c Velocity[Z] 0.14177E-38 c Pressure 0.32537E-18 0 0.10000E+01 -0.32537E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.023338 0.78886 0.12174 0.12174 v Velocity[Y] -3.8131e-18 1.8692e-17 3.247e-19 3.247e-19 v Velocity[Z] -3.5937e-18 4.4678e-18 -5.6749e-22 -5.6749e-22 v ǁVelocityǁ 0.023338 0.78886 0.12174 0.12174 v Pressure 0 0 0 0 v CourantNb 0 2.5087e-16 1.5594e-17 1.5594e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.660000000E+01 TIME STEP NUMBER 66 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13878E-11 0.14531E+00 Friction velocity uk : 0.13878E-11 0.14531E+00 Dimensionless distance yplus : 0.69391E-09 0.14531E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33706E-02 1624 0.89307E-08 0.51952E-04 0.43922E+00 c Velocity[X] 0.51952E-04 c Velocity[Y] 0.21014E-37 c Velocity[Z] 0.14467E-38 c Pressure 0.32649E-18 0 0.10000E+01 -0.32649E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.023135 0.79068 0.12192 0.12192 v Velocity[Y] -3.7279e-18 1.8718e-17 3.2769e-19 3.2769e-19 v Velocity[Z] -3.5921e-18 4.4611e-18 -9.1889e-22 -9.1889e-22 v ǁVelocityǁ 0.023135 0.79068 0.12192 0.12192 v Pressure 0 0 0 0 v CourantNb 0 2.524e-16 1.5628e-17 1.5628e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.670000000E+01 TIME STEP NUMBER 67 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13942E-11 0.14468E+00 Friction velocity uk : 0.13942E-11 0.14468E+00 Dimensionless distance yplus : 0.69712E-09 0.14468E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33800E-02 1622 0.89601E-08 0.50714E-04 0.43273E+00 c Velocity[X] 0.50714E-04 c Velocity[Y] 0.19818E-37 c Velocity[Z] 0.17753E-38 c Pressure 0.32782E-18 0 0.10000E+01 -0.32782E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.022936 0.79246 0.1221 0.1221 v Velocity[Y] -3.6455e-18 1.8742e-17 3.3059e-19 3.3059e-19 v Velocity[Z] -3.61e-18 4.4717e-18 -1.2492e-21 -1.2492e-21 v ǁVelocityǁ 0.022936 0.79246 0.1221 0.1221 v Pressure 0 0 0 0 v CourantNb 0 2.536e-16 1.5659e-17 1.5659e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.680000000E+01 TIME STEP NUMBER 68 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13282E-11 0.14406E+00 Friction velocity uk : 0.13282E-11 0.14406E+00 Dimensionless distance yplus : 0.66411E-09 0.14406E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33893E-02 1620 0.89910E-08 0.49526E-04 0.42644E+00 c Velocity[X] 0.49526E-04 c Velocity[Y] 0.18461E-37 c Velocity[Z] 0.27629E-38 c Pressure 0.32939E-18 0 0.10000E+01 -0.32939E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.022743 0.79419 0.12228 0.12228 v Velocity[Y] -3.5699e-18 1.8769e-17 3.3342e-19 3.3342e-19 v Velocity[Z] -3.6214e-18 4.5222e-18 -9.9183e-22 -9.9183e-22 v ǁVelocityǁ 0.022743 0.79419 0.12228 0.12228 v Pressure 0 0 0 0 v CourantNb 0 2.5413e-16 1.5688e-17 1.5688e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.690000000E+01 TIME STEP NUMBER 69 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14566E-11 0.14346E+00 Friction velocity uk : 0.14566E-11 0.14346E+00 Dimensionless distance yplus : 0.72829E-09 0.14346E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.33984E-02 1619 0.89512E-08 0.48383E-04 0.42033E+00 c Velocity[X] 0.48383E-04 c Velocity[Y] 0.17618E-37 c Velocity[Z] 0.24452E-38 c Pressure 0.33046E-18 0 0.10000E+01 -0.33046E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.022555 0.79587 0.12245 0.12245 v Velocity[Y] -3.4968e-18 1.8793e-17 3.3618e-19 3.3618e-19 v Velocity[Z] -3.6168e-18 4.551e-18 -7.9367e-22 -7.9367e-22 v ǁVelocityǁ 0.022555 0.79587 0.12245 0.12245 v Pressure 0 0 0 0 v CourantNb 0 2.5546e-16 1.574e-17 1.574e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.700000000E+01 TIME STEP NUMBER 70 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14392E-11 0.14287E+00 Friction velocity uk : 0.14392E-11 0.14287E+00 Dimensionless distance yplus : 0.71960E-09 0.14287E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34075E-02 1617 0.89851E-08 0.47284E-04 0.41440E+00 c Velocity[X] 0.47284E-04 c Velocity[Y] 0.16907E-37 c Velocity[Z] 0.14392E-38 c Pressure 0.33167E-18 0 0.10000E+01 -0.33167E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.022371 0.79752 0.12263 0.12263 v Velocity[Y] -3.4231e-18 1.8814e-17 3.3886e-19 3.3886e-19 v Velocity[Z] -3.6419e-18 4.5748e-18 -5.126e-22 -5.126e-22 v ǁVelocityǁ 0.022371 0.79752 0.12263 0.12263 v Pressure 0 0 0 0 v CourantNb 0 2.561e-16 1.5781e-17 1.5781e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.710000000E+01 TIME STEP NUMBER 71 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15856E-11 0.14230E+00 Friction velocity uk : 0.15856E-11 0.14230E+00 Dimensionless distance yplus : 0.79278E-09 0.14230E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34164E-02 1616 0.89482E-08 0.46225E-04 0.40864E+00 c Velocity[X] 0.46225E-04 c Velocity[Y] 0.16697E-37 c Velocity[Z] 0.12969E-38 c Pressure 0.33310E-18 0 0.10000E+01 -0.33310E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.022192 0.79912 0.1228 0.1228 v Velocity[Y] -3.347e-18 1.8829e-17 3.4148e-19 3.4148e-19 v Velocity[Z] -3.657e-18 4.5937e-18 -7.8756e-22 -7.8756e-22 v ǁVelocityǁ 0.022192 0.79912 0.1228 0.1228 v Pressure 0 0 0 0 v CourantNb 0 2.5675e-16 1.5829e-17 1.5829e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.720000000E+01 TIME STEP NUMBER 72 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13532E-11 0.14173E+00 Friction velocity uk : 0.13532E-11 0.14173E+00 Dimensionless distance yplus : 0.67659E-09 0.14173E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34252E-02 1614 0.89849E-08 0.45206E-04 0.40305E+00 c Velocity[X] 0.45206E-04 c Velocity[Y] 0.16210E-37 c Velocity[Z] 0.13861E-38 c Pressure 0.33426E-18 0 0.10000E+01 -0.33426E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.022017 0.80069 0.12297 0.12297 v Velocity[Y] -3.2753e-18 1.8845e-17 3.4402e-19 3.4402e-19 v Velocity[Z] -3.655e-18 4.6056e-18 -6.7948e-22 -6.7948e-22 v ǁVelocityǁ 0.022017 0.80069 0.12297 0.12297 v Pressure 0 0 0 0 v CourantNb 0 2.5853e-16 1.5867e-17 1.5867e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.730000000E+01 TIME STEP NUMBER 73 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13540E-11 0.14118E+00 Friction velocity uk : 0.13540E-11 0.14118E+00 Dimensionless distance yplus : 0.67700E-09 0.14118E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34339E-02 1613 0.89507E-08 0.44224E-04 0.39761E+00 c Velocity[X] 0.44224E-04 c Velocity[Y] 0.15951E-37 c Velocity[Z] 0.17017E-38 c Pressure 0.33546E-18 0 0.10000E+01 -0.33546E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.021846 0.80222 0.12315 0.12315 v Velocity[Y] -3.2017e-18 1.8857e-17 3.4649e-19 3.4649e-19 v Velocity[Z] -3.6734e-18 4.6066e-18 -8.4485e-22 -8.4485e-22 v ǁVelocityǁ 0.021846 0.80222 0.12315 0.12315 v Pressure 0 0 0 0 v CourantNb 0 2.5949e-16 1.5903e-17 1.5903e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.740000000E+01 TIME STEP NUMBER 74 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12284E-11 0.14064E+00 Friction velocity uk : 0.12284E-11 0.14064E+00 Dimensionless distance yplus : 0.61420E-09 0.14064E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34425E-02 1611 0.89901E-08 0.43277E-04 0.39232E+00 c Velocity[X] 0.43277E-04 c Velocity[Y] 0.13909E-37 c Velocity[Z] 0.20064E-38 c Pressure 0.33684E-18 0 0.10000E+01 -0.33684E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.021679 0.80371 0.12331 0.12331 v Velocity[Y] -3.1366e-18 1.8873e-17 3.489e-19 3.489e-19 v Velocity[Z] -3.681e-18 4.6389e-18 -5.9374e-22 -5.9374e-22 v ǁVelocityǁ 0.021679 0.80371 0.12331 0.12331 v Pressure 0 0 0 0 v CourantNb 0 2.6042e-16 1.5942e-17 1.5942e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.750000000E+01 TIME STEP NUMBER 75 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12691E-11 0.14010E+00 Friction velocity uk : 0.12691E-11 0.14010E+00 Dimensionless distance yplus : 0.63454E-09 0.14010E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34511E-02 1610 0.89585E-08 0.42364E-04 0.38718E+00 c Velocity[X] 0.42364E-04 c Velocity[Y] 0.13670E-37 c Velocity[Z] 0.13322E-38 c Pressure 0.33794E-18 0 0.10000E+01 -0.33794E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.021516 0.80517 0.12348 0.12348 v Velocity[Y] -3.0713e-18 1.8887e-17 3.5124e-19 3.5124e-19 v Velocity[Z] -3.6848e-18 4.6492e-18 -4.4694e-22 -4.4694e-22 v ǁVelocityǁ 0.021516 0.80517 0.12348 0.12348 v Pressure 0 0 0 0 v CourantNb 0 2.6021e-16 1.5972e-17 1.5972e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.760000000E+01 TIME STEP NUMBER 76 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12247E-11 0.13958E+00 Friction velocity uk : 0.12247E-11 0.13958E+00 Dimensionless distance yplus : 0.61236E-09 0.13958E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34595E-02 1608 0.90004E-08 0.41482E-04 0.38217E+00 c Velocity[X] 0.41482E-04 c Velocity[Y] 0.13573E-37 c Velocity[Z] 0.15140E-38 c Pressure 0.33917E-18 0 0.10000E+01 -0.33917E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.021357 0.80659 0.12365 0.12365 v Velocity[Y] -3.0047e-18 1.8897e-17 3.5352e-19 3.5352e-19 v Velocity[Z] -3.6965e-18 4.6503e-18 -6.7695e-22 -6.7695e-22 v ǁVelocityǁ 0.021357 0.80659 0.12365 0.12365 v Pressure 0 0 0 0 v CourantNb 0 2.6134e-16 1.601e-17 1.601e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.770000000E+01 TIME STEP NUMBER 77 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13355E-11 0.13907E+00 Friction velocity uk : 0.13355E-11 0.13907E+00 Dimensionless distance yplus : 0.66776E-09 0.13907E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34678E-02 1607 0.89713E-08 0.40630E-04 0.37730E+00 c Velocity[X] 0.40630E-04 c Velocity[Y] 0.13191E-37 c Velocity[Z] 0.15998E-38 c Pressure 0.34010E-18 0 0.10000E+01 -0.34010E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.021201 0.80799 0.12382 0.12382 v Velocity[Y] -2.9386e-18 1.8903e-17 3.5574e-19 3.5574e-19 v Velocity[Z] -3.7022e-18 4.6546e-18 -7.3786e-22 -7.3786e-22 v ǁVelocityǁ 0.021201 0.80799 0.12382 0.12382 v Pressure 0 0 0 0 v CourantNb 0 2.6242e-16 1.6034e-17 1.6034e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.780000000E+01 TIME STEP NUMBER 78 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13574E-11 0.13857E+00 Friction velocity uk : 0.13574E-11 0.13857E+00 Dimensionless distance yplus : 0.67869E-09 0.13857E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34761E-02 1606 0.89434E-08 0.39807E-04 0.37255E+00 c Velocity[X] 0.39807E-04 c Velocity[Y] 0.12767E-37 c Velocity[Z] 0.19041E-38 c Pressure 0.34143E-18 0 0.10000E+01 -0.34143E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.021049 0.80935 0.12398 0.12398 v Velocity[Y] -2.8733e-18 1.8909e-17 3.5789e-19 3.5789e-19 v Velocity[Z] -3.7009e-18 4.6824e-18 -7.6206e-22 -7.6206e-22 v ǁVelocityǁ 0.021049 0.80935 0.12398 0.12398 v Pressure 0 0 0 0 v CourantNb 0 2.6393e-16 1.6058e-17 1.6058e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.790000000E+01 TIME STEP NUMBER 79 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14447E-11 0.13808E+00 Friction velocity uk : 0.14447E-11 0.13808E+00 Dimensionless distance yplus : 0.72235E-09 0.13808E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34842E-02 1604 0.89889E-08 0.39012E-04 0.36793E+00 c Velocity[X] 0.39012E-04 c Velocity[Y] 0.12446E-37 c Velocity[Z] 0.16257E-38 c Pressure 0.34255E-18 0 0.10000E+01 -0.34255E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0209 0.81068 0.12414 0.12414 v Velocity[Y] -2.8084e-18 1.8914e-17 3.5998e-19 3.5998e-19 v Velocity[Z] -3.7217e-18 4.6943e-18 -9.2549e-22 -9.2549e-22 v ǁVelocityǁ 0.0209 0.81068 0.12414 0.12414 v Pressure 0 0 0 0 v CourantNb 0 2.6453e-16 1.61e-17 1.61e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.800000000E+01 TIME STEP NUMBER 80 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14067E-11 0.13759E+00 Friction velocity uk : 0.14067E-11 0.13759E+00 Dimensionless distance yplus : 0.70336E-09 0.13759E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.34923E-02 1603 0.89633E-08 0.38243E-04 0.36342E+00 c Velocity[X] 0.38243E-04 c Velocity[Y] 0.12280E-37 c Velocity[Z] 0.32025E-38 c Pressure 0.34372E-18 0 0.10000E+01 -0.34372E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.020754 0.81199 0.12431 0.12431 v Velocity[Y] -2.7459e-18 1.8919e-17 3.6202e-19 3.6202e-19 v Velocity[Z] -3.7222e-18 4.7035e-18 -8.5935e-22 -8.5935e-22 v ǁVelocityǁ 0.020754 0.81199 0.12431 0.12431 v Pressure 0 0 0 0 v CourantNb 0 2.6482e-16 1.6126e-17 1.6126e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.810000000E+01 TIME STEP NUMBER 81 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16441E-11 0.13712E+00 Friction velocity uk : 0.16441E-11 0.13712E+00 Dimensionless distance yplus : 0.82203E-09 0.13712E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35003E-02 1602 0.89388E-08 0.37498E-04 0.35902E+00 c Velocity[X] 0.37498E-04 c Velocity[Y] 0.11535E-37 c Velocity[Z] 0.30544E-38 c Pressure 0.34511E-18 0 0.10000E+01 -0.34511E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.020611 0.81326 0.12447 0.12447 v Velocity[Y] -2.6846e-18 1.8921e-17 3.6399e-19 3.6399e-19 v Velocity[Z] -3.7449e-18 4.7492e-18 -9.3836e-22 -9.3836e-22 v ǁVelocityǁ 0.020611 0.81326 0.12447 0.12447 v Pressure 0 0 0 0 v CourantNb 0 2.6587e-16 1.6184e-17 1.6184e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.820000000E+01 TIME STEP NUMBER 82 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12566E-11 0.13665E+00 Friction velocity uk : 0.12566E-11 0.13665E+00 Dimensionless distance yplus : 0.62830E-09 0.13665E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35082E-02 1600 0.89876E-08 0.36778E-04 0.35473E+00 c Velocity[X] 0.36778E-04 c Velocity[Y] 0.11376E-37 c Velocity[Z] 0.14672E-38 c Pressure 0.34602E-18 0 0.10000E+01 -0.34602E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.020471 0.81452 0.12463 0.12463 v Velocity[Y] -2.624e-18 1.8918e-17 3.659e-19 3.659e-19 v Velocity[Z] -3.7459e-18 4.7431e-18 -8.852e-22 -8.852e-22 v ǁVelocityǁ 0.020471 0.81452 0.12463 0.12463 v Pressure 0 0 0 0 v CourantNb 0 2.6795e-16 1.6241e-17 1.6241e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.830000000E+01 TIME STEP NUMBER 83 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17024E-11 0.13619E+00 Friction velocity uk : 0.17024E-11 0.13619E+00 Dimensionless distance yplus : 0.85121E-09 0.13619E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35160E-02 1599 0.89652E-08 0.36080E-04 0.35055E+00 c Velocity[X] 0.36080E-04 c Velocity[Y] 0.11114E-37 c Velocity[Z] 0.13658E-38 c Pressure 0.34708E-18 0 0.10000E+01 -0.34708E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.020334 0.81574 0.12479 0.12479 v Velocity[Y] -2.5631e-18 1.8914e-17 3.6776e-19 3.6776e-19 v Velocity[Z] -3.7481e-18 4.7443e-18 -9.9229e-22 -9.9229e-22 v ǁVelocityǁ 0.020334 0.81574 0.12479 0.12479 v Pressure 0 0 0 0 v CourantNb 0 2.6742e-16 1.6249e-17 1.6249e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.840000000E+01 TIME STEP NUMBER 84 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16292E-11 0.13574E+00 Friction velocity uk : 0.16292E-11 0.13574E+00 Dimensionless distance yplus : 0.81461E-09 0.13574E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35238E-02 1598 0.89439E-08 0.35404E-04 0.34647E+00 c Velocity[X] 0.35404E-04 c Velocity[Y] 0.11577E-37 c Velocity[Z] 0.12143E-38 c Pressure 0.34825E-18 0 0.10000E+01 -0.34825E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.020199 0.81694 0.12494 0.12494 v Velocity[Y] -2.5003e-18 1.8907e-17 3.6955e-19 3.6955e-19 v Velocity[Z] -3.7655e-18 4.7581e-18 -1.2011e-21 -1.2011e-21 v ǁVelocityǁ 0.020199 0.81694 0.12494 0.12494 v Pressure 0 0 0 0 v CourantNb 0 2.6838e-16 1.6279e-17 1.6279e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.850000000E+01 TIME STEP NUMBER 85 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17425E-11 0.13530E+00 Friction velocity uk : 0.17425E-11 0.13530E+00 Dimensionless distance yplus : 0.87127E-09 0.13530E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35314E-02 1596 0.89958E-08 0.34749E-04 0.34248E+00 c Velocity[X] 0.34749E-04 c Velocity[Y] 0.99543E-38 c Velocity[Z] 0.21168E-38 c Pressure 0.34926E-18 0 0.10000E+01 -0.34926E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.020068 0.81812 0.1251 0.1251 v Velocity[Y] -2.4465e-18 1.8905e-17 3.713e-19 3.713e-19 v Velocity[Z] -3.7461e-18 4.7978e-18 -8.595e-22 -8.595e-22 v ǁVelocityǁ 0.020068 0.81812 0.1251 0.1251 v Pressure 0 0 0 0 v CourantNb 0 2.6877e-16 1.63e-17 1.63e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.860000000E+01 TIME STEP NUMBER 86 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16091E-11 0.13486E+00 Friction velocity uk : 0.16091E-11 0.13486E+00 Dimensionless distance yplus : 0.80457E-09 0.13486E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35391E-02 1595 0.89764E-08 0.34114E-04 0.33859E+00 c Velocity[X] 0.34114E-04 c Velocity[Y] 0.95587E-38 c Velocity[Z] 0.13967E-38 c Pressure 0.35031E-18 0 0.10000E+01 -0.35031E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.019939 0.81927 0.12526 0.12526 v Velocity[Y] -2.3897e-18 1.8901e-17 3.7298e-19 3.7298e-19 v Velocity[Z] -3.7598e-18 4.7766e-18 -1.3118e-21 -1.3118e-21 v ǁVelocityǁ 0.019939 0.81927 0.12526 0.12526 v Pressure 0 0 0 0 v CourantNb 0 2.689e-16 1.6331e-17 1.6331e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.870000000E+01 TIME STEP NUMBER 87 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14545E-11 0.13444E+00 Friction velocity uk : 0.14545E-11 0.13444E+00 Dimensionless distance yplus : 0.72723E-09 0.13444E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35466E-02 1594 0.89581E-08 0.33498E-04 0.33478E+00 c Velocity[X] 0.33498E-04 c Velocity[Y] 0.90290E-38 c Velocity[Z] 0.39888E-38 c Pressure 0.35147E-18 0 0.10000E+01 -0.35147E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.019812 0.8204 0.12541 0.12541 v Velocity[Y] -2.3422e-18 1.8902e-17 3.7462e-19 3.7462e-19 v Velocity[Z] -3.7606e-18 4.8411e-18 -6.2525e-22 -6.2525e-22 v ǁVelocityǁ 0.019812 0.8204 0.12541 0.12541 v Pressure 0 0 0 0 v CourantNb 0 2.7027e-16 1.6359e-17 1.6359e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.880000000E+01 TIME STEP NUMBER 88 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12883E-11 0.13401E+00 Friction velocity uk : 0.12883E-11 0.13401E+00 Dimensionless distance yplus : 0.64416E-09 0.13401E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35541E-02 1592 0.90130E-08 0.32900E-04 0.33107E+00 c Velocity[X] 0.32900E-04 c Velocity[Y] 0.80167E-38 c Velocity[Z] 0.18743E-38 c Pressure 0.35266E-18 0 0.10000E+01 -0.35266E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.019688 0.82151 0.12557 0.12557 v Velocity[Y] -2.2946e-18 1.8903e-17 3.7622e-19 3.7622e-19 v Velocity[Z] -3.7659e-18 4.8495e-18 -4.1608e-22 -4.1608e-22 v ǁVelocityǁ 0.019688 0.82151 0.12557 0.12557 v Pressure 0 0 0 0 v CourantNb 0 2.7028e-16 1.64e-17 1.64e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.890000000E+01 TIME STEP NUMBER 89 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12329E-11 0.13360E+00 Friction velocity uk : 0.12329E-11 0.13360E+00 Dimensionless distance yplus : 0.61647E-09 0.13360E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35614E-02 1591 0.89964E-08 0.32320E-04 0.32744E+00 c Velocity[X] 0.32320E-04 c Velocity[Y] 0.84648E-38 c Velocity[Z] 0.21797E-38 c Pressure 0.35368E-18 0 0.10000E+01 -0.35368E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.019566 0.8226 0.12572 0.12572 v Velocity[Y] -2.2424e-18 1.8896e-17 3.7776e-19 3.7776e-19 v Velocity[Z] -3.7677e-18 4.8671e-18 -2.9443e-22 -2.9443e-22 v ǁVelocityǁ 0.019566 0.8226 0.12572 0.12572 v Pressure 0 0 0 0 v CourantNb 0 2.7055e-16 1.6438e-17 1.6438e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.900000000E+01 TIME STEP NUMBER 90 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11234E-11 0.13319E+00 Friction velocity uk : 0.11234E-11 0.13319E+00 Dimensionless distance yplus : 0.56169E-09 0.13319E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35688E-02 1590 0.89808E-08 0.31757E-04 0.32389E+00 c Velocity[X] 0.31757E-04 c Velocity[Y] 0.76716E-38 c Velocity[Z] 0.14574E-38 c Pressure 0.35476E-18 0 0.10000E+01 -0.35476E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.019447 0.82367 0.12587 0.12587 v Velocity[Y] -2.1958e-18 1.8891e-17 3.7926e-19 3.7926e-19 v Velocity[Z] -3.7891e-18 4.8713e-18 -1.473e-22 -1.473e-22 v ǁVelocityǁ 0.019447 0.82367 0.12587 0.12587 v Pressure 0 0 0 0 v CourantNb 0 2.7228e-16 1.6483e-17 1.6483e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.910000000E+01 TIME STEP NUMBER 91 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12349E-11 0.13279E+00 Friction velocity uk : 0.12349E-11 0.13279E+00 Dimensionless distance yplus : 0.61745E-09 0.13279E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35760E-02 1589 0.89661E-08 0.31210E-04 0.32041E+00 c Velocity[X] 0.31210E-04 c Velocity[Y] 0.82019E-38 c Velocity[Z] 0.14635E-38 c Pressure 0.35577E-18 0 0.10000E+01 -0.35577E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.019329 0.82472 0.12602 0.12602 v Velocity[Y] -2.1461e-18 1.8882e-17 3.8071e-19 3.8071e-19 v Velocity[Z] -3.7937e-18 4.8745e-18 -5.2256e-22 -5.2256e-22 v ǁVelocityǁ 0.019329 0.82472 0.12602 0.12602 v Pressure 0 0 0 0 v CourantNb 0 2.7226e-16 1.6502e-17 1.6502e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.920000000E+01 TIME STEP NUMBER 92 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13058E-11 0.13239E+00 Friction velocity uk : 0.13058E-11 0.13239E+00 Dimensionless distance yplus : 0.65290E-09 0.13239E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35832E-02 1588 0.89523E-08 0.30678E-04 0.31702E+00 c Velocity[X] 0.30678E-04 c Velocity[Y] 0.83165E-38 c Velocity[Z] 0.21560E-38 c Pressure 0.35689E-18 0 0.10000E+01 -0.35689E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.019214 0.82575 0.12617 0.12617 v Velocity[Y] -2.0941e-18 1.8872e-17 3.8211e-19 3.8211e-19 v Velocity[Z] -3.8382e-18 4.877e-18 -7.3711e-22 -7.3711e-22 v ǁVelocityǁ 0.019214 0.82575 0.12617 0.12617 v Pressure 0 0 0 0 v CourantNb 0 2.7246e-16 1.6536e-17 1.6536e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.930000000E+01 TIME STEP NUMBER 93 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16110E-11 0.13200E+00 Friction velocity uk : 0.16110E-11 0.13200E+00 Dimensionless distance yplus : 0.80548E-09 0.13200E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35904E-02 1586 0.90116E-08 0.30161E-04 0.31369E+00 c Velocity[X] 0.30161E-04 c Velocity[Y] 0.77528E-38 c Velocity[Z] 0.16207E-38 c Pressure 0.35771E-18 0 0.10000E+01 -0.35771E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.019101 0.82676 0.12632 0.12632 v Velocity[Y] -2.046e-18 1.8864e-17 3.8347e-19 3.8347e-19 v Velocity[Z] -3.8212e-18 4.9007e-18 -6.3188e-22 -6.3188e-22 v ǁVelocityǁ 0.019101 0.82676 0.12632 0.12632 v Pressure 0 0 0 0 v CourantNb 0 2.7435e-16 1.6571e-17 1.6571e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.940000000E+01 TIME STEP NUMBER 94 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17554E-11 0.13162E+00 Friction velocity uk : 0.17554E-11 0.13162E+00 Dimensionless distance yplus : 0.87770E-09 0.13162E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.35975E-02 1585 0.89994E-08 0.29659E-04 0.31044E+00 c Velocity[X] 0.29659E-04 c Velocity[Y] 0.79854E-38 c Velocity[Z] 0.11459E-38 c Pressure 0.35874E-18 0 0.10000E+01 -0.35874E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018989 0.82775 0.12647 0.12647 v Velocity[Y] -1.9973e-18 1.8852e-17 3.8478e-19 3.8478e-19 v Velocity[Z] -3.8144e-18 4.914e-18 -6.6753e-22 -6.6753e-22 v ǁVelocityǁ 0.018989 0.82775 0.12647 0.12647 v Pressure 0 0 0 0 v CourantNb 0 2.7523e-16 1.6604e-17 1.6604e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.950000000E+01 TIME STEP NUMBER 95 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18404E-11 0.13124E+00 Friction velocity uk : 0.18404E-11 0.13124E+00 Dimensionless distance yplus : 0.92020E-09 0.13124E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36045E-02 1584 0.89881E-08 0.29170E-04 0.30725E+00 c Velocity[X] 0.29170E-04 c Velocity[Y] 0.80847E-38 c Velocity[Z] 0.18868E-38 c Pressure 0.35978E-18 0 0.10000E+01 -0.35978E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01888 0.82873 0.12662 0.12662 v Velocity[Y] -1.947e-18 1.8837e-17 3.8604e-19 3.8604e-19 v Velocity[Z] -3.8429e-18 4.8961e-18 -4.8573e-22 -4.8573e-22 v ǁVelocityǁ 0.01888 0.82873 0.12662 0.12662 v Pressure 0 0 0 0 v CourantNb 0 2.761e-16 1.6629e-17 1.6629e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.960000000E+01 TIME STEP NUMBER 96 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18936E-11 0.13087E+00 Friction velocity uk : 0.18936E-11 0.13087E+00 Dimensionless distance yplus : 0.94682E-09 0.13087E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36114E-02 1583 0.89776E-08 0.28694E-04 0.30414E+00 c Velocity[X] 0.28694E-04 c Velocity[Y] 0.73611E-38 c Velocity[Z] 0.27428E-38 c Pressure 0.36055E-18 0 0.10000E+01 -0.36055E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018773 0.82969 0.12676 0.12676 v Velocity[Y] -1.9012e-18 1.8823e-17 3.8726e-19 3.8726e-19 v Velocity[Z] -3.8347e-18 4.9228e-18 -7.0268e-22 -7.0268e-22 v ǁVelocityǁ 0.018773 0.82969 0.12676 0.12676 v Pressure 0 0 0 0 v CourantNb 0 2.7592e-16 1.6644e-17 1.6644e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.970000000E+01 TIME STEP NUMBER 97 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21246E-11 0.13050E+00 Friction velocity uk : 0.21246E-11 0.13050E+00 Dimensionless distance yplus : 0.10623E-08 0.13050E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36183E-02 1582 0.89679E-08 0.28232E-04 0.30108E+00 c Velocity[X] 0.28232E-04 c Velocity[Y] 0.68292E-38 c Velocity[Z] 0.12114E-38 c Pressure 0.36154E-18 0 0.10000E+01 -0.36154E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018667 0.83063 0.12691 0.12691 v Velocity[Y] -1.8564e-18 1.881e-17 3.8843e-19 3.8843e-19 v Velocity[Z] -3.8457e-18 4.9229e-18 -8.8775e-22 -8.8775e-22 v ǁVelocityǁ 0.018667 0.83063 0.12691 0.12691 v Pressure 0 0 0 0 v CourantNb 0 2.7778e-16 1.6691e-17 1.6691e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.980000000E+01 TIME STEP NUMBER 98 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21570E-11 0.13014E+00 Friction velocity uk : 0.21570E-11 0.13014E+00 Dimensionless distance yplus : 0.10785E-08 0.13014E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36252E-02 1581 0.89589E-08 0.27781E-04 0.29809E+00 c Velocity[X] 0.27781E-04 c Velocity[Y] 0.67431E-38 c Velocity[Z] 0.13229E-38 c Pressure 0.36254E-18 0 0.10000E+01 -0.36254E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018563 0.83156 0.12705 0.12705 v Velocity[Y] -1.8137e-18 1.8797e-17 3.8957e-19 3.8957e-19 v Velocity[Z] -3.8753e-18 4.9221e-18 -1.0701e-21 -1.0701e-21 v ǁVelocityǁ 0.018563 0.83156 0.12705 0.12705 v Pressure 0 0 0 0 v CourantNb 0 2.7872e-16 1.6723e-17 1.6723e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.990000000E+01 TIME STEP NUMBER 99 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19768E-11 0.12979E+00 Friction velocity uk : 0.19768E-11 0.12979E+00 Dimensionless distance yplus : 0.98842E-09 0.12979E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36320E-02 1579 0.90230E-08 0.27343E-04 0.29516E+00 c Velocity[X] 0.27343E-04 c Velocity[Y] 0.71805E-38 c Velocity[Z] 0.16992E-38 c Pressure 0.36343E-18 0 0.10000E+01 -0.36343E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018461 0.83247 0.1272 0.1272 v Velocity[Y] -1.7678e-18 1.8779e-17 3.9066e-19 3.9066e-19 v Velocity[Z] -3.8482e-18 4.9475e-18 -1.0003e-21 -1.0003e-21 v ǁVelocityǁ 0.018461 0.83247 0.1272 0.1272 v Pressure 0 0 0 0 v CourantNb 0 2.7929e-16 1.6754e-17 1.6754e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.100000000E+02 TIME STEP NUMBER 100 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19446E-11 0.12943E+00 Friction velocity uk : 0.19446E-11 0.12943E+00 Dimensionless distance yplus : 0.97232E-09 0.12943E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 100, Physical time 0.10000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36387E-02 1578 0.90155E-08 0.26915E-04 0.29229E+00 c Velocity[X] 0.26915E-04 c Velocity[Y] 0.68496E-38 c Velocity[Z] 0.14688E-38 c Pressure 0.36469E-18 0 0.10000E+01 -0.36469E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018361 0.83337 0.12734 0.12734 v Velocity[Y] -1.7236e-18 1.8762e-17 3.917e-19 3.917e-19 v Velocity[Z] -3.8707e-18 4.9644e-18 -9.4552e-22 -9.4552e-22 v ǁVelocityǁ 0.018361 0.83337 0.12734 0.12734 v Pressure 0 0 0 0 v CourantNb 0 2.7846e-16 1.676e-17 1.676e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.101000000E+02 TIME STEP NUMBER 101 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19488E-11 0.12909E+00 Friction velocity uk : 0.19488E-11 0.12909E+00 Dimensionless distance yplus : 0.97441E-09 0.12909E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36454E-02 1577 0.90087E-08 0.26499E-04 0.28947E+00 c Velocity[X] 0.26499E-04 c Velocity[Y] 0.63502E-38 c Velocity[Z] 0.16806E-38 c Pressure 0.36544E-18 0 0.10000E+01 -0.36544E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018262 0.83425 0.12748 0.12748 v Velocity[Y] -1.6812e-18 1.8745e-17 3.9271e-19 3.9271e-19 v Velocity[Z] -3.8718e-18 4.9556e-18 -8.337e-22 -8.337e-22 v ǁVelocityǁ 0.018262 0.83425 0.12748 0.12748 v Pressure 0 0 0 0 v CourantNb 0 2.786e-16 1.6782e-17 1.6782e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.102000000E+02 TIME STEP NUMBER 102 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19933E-11 0.12874E+00 Friction velocity uk : 0.19933E-11 0.12874E+00 Dimensionless distance yplus : 0.99664E-09 0.12874E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36520E-02 1576 0.90027E-08 0.26094E-04 0.28671E+00 c Velocity[X] 0.26094E-04 c Velocity[Y] 0.53288E-38 c Velocity[Z] 0.26479E-38 c Pressure 0.36656E-18 0 0.10000E+01 -0.36656E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018165 0.83512 0.12762 0.12762 v Velocity[Y] -1.6469e-18 1.8733e-17 3.9369e-19 3.9369e-19 v Velocity[Z] -3.8746e-18 5.015e-18 -9.1984e-22 -9.1984e-22 v ǁVelocityǁ 0.018165 0.83512 0.12762 0.12762 v Pressure 0 0 0 0 v CourantNb 0 2.8001e-16 1.6809e-17 1.6809e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.103000000E+02 TIME STEP NUMBER 103 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13602E-11 0.12841E+00 Friction velocity uk : 0.13602E-11 0.12841E+00 Dimensionless distance yplus : 0.68008E-09 0.12841E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36586E-02 1575 0.89974E-08 0.25698E-04 0.28400E+00 c Velocity[X] 0.25698E-04 c Velocity[Y] 0.61616E-38 c Velocity[Z] 0.18181E-38 c Pressure 0.36744E-18 0 0.10000E+01 -0.36744E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.018069 0.83597 0.12776 0.12776 v Velocity[Y] -1.6449e-18 1.8716e-17 3.9462e-19 3.9462e-19 v Velocity[Z] -3.8915e-18 5.0017e-18 -6.2697e-22 -6.2697e-22 v ǁVelocityǁ 0.018069 0.83597 0.12776 0.12776 v Pressure 0 0 0 0 v CourantNb 0 2.8033e-16 1.6858e-17 1.6858e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.104000000E+02 TIME STEP NUMBER 104 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18192E-11 0.12807E+00 Friction velocity uk : 0.18192E-11 0.12807E+00 Dimensionless distance yplus : 0.90961E-09 0.12807E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36651E-02 1574 0.89927E-08 0.25312E-04 0.28134E+00 c Velocity[X] 0.25312E-04 c Velocity[Y] 0.56725E-38 c Velocity[Z] 0.17733E-38 c Pressure 0.36830E-18 0 0.10000E+01 -0.36830E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017975 0.83681 0.1279 0.1279 v Velocity[Y] -1.652e-18 1.8701e-17 3.9552e-19 3.9552e-19 v Velocity[Z] -3.8921e-18 5.0317e-18 -5.8971e-22 -5.8971e-22 v ǁVelocityǁ 0.017975 0.83681 0.1279 0.1279 v Pressure 0 0 0 0 v CourantNb 0 2.8048e-16 1.6891e-17 1.6891e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.105000000E+02 TIME STEP NUMBER 105 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18184E-11 0.12775E+00 Friction velocity uk : 0.18184E-11 0.12775E+00 Dimensionless distance yplus : 0.90919E-09 0.12775E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36716E-02 1573 0.89888E-08 0.24936E-04 0.27874E+00 c Velocity[X] 0.24936E-04 c Velocity[Y] 0.55688E-38 c Velocity[Z] 0.20203E-38 c Pressure 0.36940E-18 0 0.10000E+01 -0.36940E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017882 0.83764 0.12804 0.12804 v Velocity[Y] -1.6595e-18 1.8687e-17 3.9638e-19 3.9638e-19 v Velocity[Z] -3.8927e-18 5.0263e-18 -5.1065e-22 -5.1065e-22 v ǁVelocityǁ 0.017882 0.83764 0.12804 0.12804 v Pressure 0 0 0 0 v CourantNb 0 2.8165e-16 1.6929e-17 1.6929e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.106000000E+02 TIME STEP NUMBER 106 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18135E-11 0.12742E+00 Friction velocity uk : 0.18135E-11 0.12742E+00 Dimensionless distance yplus : 0.90676E-09 0.12742E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36781E-02 1572 0.89855E-08 0.24569E-04 0.27618E+00 c Velocity[X] 0.24569E-04 c Velocity[Y] 0.51420E-38 c Velocity[Z] 0.15071E-38 c Pressure 0.37016E-18 0 0.10000E+01 -0.37016E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017791 0.83845 0.12818 0.12818 v Velocity[Y] -1.6666e-18 1.8669e-17 3.9722e-19 3.9722e-19 v Velocity[Z] -3.8747e-18 5.0394e-18 -5.3806e-22 -5.3806e-22 v ǁVelocityǁ 0.017791 0.83845 0.12818 0.12818 v Pressure 0 0 0 0 v CourantNb 0 2.8196e-16 1.6953e-17 1.6953e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.107000000E+02 TIME STEP NUMBER 107 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16558E-11 0.12710E+00 Friction velocity uk : 0.16558E-11 0.12710E+00 Dimensionless distance yplus : 0.82788E-09 0.12710E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36844E-02 1571 0.89829E-08 0.24211E-04 0.27367E+00 c Velocity[X] 0.24211E-04 c Velocity[Y] 0.50667E-38 c Velocity[Z] 0.13252E-38 c Pressure 0.37112E-18 0 0.10000E+01 -0.37112E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017701 0.83925 0.12832 0.12832 v Velocity[Y] -1.6737e-18 1.8653e-17 3.9801e-19 3.9801e-19 v Velocity[Z] -3.9003e-18 5.0325e-18 -6.3513e-22 -6.3513e-22 v ǁVelocityǁ 0.017701 0.83925 0.12832 0.12832 v Pressure 0 0 0 0 v CourantNb 0 2.8191e-16 1.6966e-17 1.6966e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.108000000E+02 TIME STEP NUMBER 108 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15556E-11 0.12679E+00 Friction velocity uk : 0.15556E-11 0.12679E+00 Dimensionless distance yplus : 0.77781E-09 0.12679E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36908E-02 1570 0.89809E-08 0.23862E-04 0.27121E+00 c Velocity[X] 0.23862E-04 c Velocity[Y] 0.54543E-38 c Velocity[Z] 0.22573E-38 c Pressure 0.37203E-18 0 0.10000E+01 -0.37203E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017613 0.84004 0.12846 0.12846 v Velocity[Y] -1.6813e-18 1.8635e-17 3.9877e-19 3.9877e-19 v Velocity[Z] -3.9219e-18 5.0632e-18 -4.5816e-22 -4.5816e-22 v ǁVelocityǁ 0.017613 0.84004 0.12846 0.12846 v Pressure 0 0 0 0 v CourantNb 0 2.8264e-16 1.6997e-17 1.6997e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.109000000E+02 TIME STEP NUMBER 109 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15319E-11 0.12647E+00 Friction velocity uk : 0.15319E-11 0.12647E+00 Dimensionless distance yplus : 0.76593E-09 0.12647E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.36971E-02 1569 0.89795E-08 0.23521E-04 0.26879E+00 c Velocity[X] 0.23521E-04 c Velocity[Y] 0.55683E-38 c Velocity[Z] 0.12915E-38 c Pressure 0.37305E-18 0 0.10000E+01 -0.37305E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017525 0.84082 0.12859 0.12859 v Velocity[Y] -1.6891e-18 1.8615e-17 3.995e-19 3.995e-19 v Velocity[Z] -3.9345e-18 5.063e-18 -1.0993e-21 -1.0993e-21 v ǁVelocityǁ 0.017525 0.84082 0.12859 0.12859 v Pressure 0 0 0 0 v CourantNb 0 2.838e-16 1.7045e-17 1.7045e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.110000000E+02 TIME STEP NUMBER 110 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15018E-11 0.12617E+00 Friction velocity uk : 0.15018E-11 0.12617E+00 Dimensionless distance yplus : 0.75091E-09 0.12617E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37033E-02 1568 0.89788E-08 0.23188E-04 0.26642E+00 c Velocity[X] 0.23188E-04 c Velocity[Y] 0.46823E-38 c Velocity[Z] 0.16817E-38 c Pressure 0.37380E-18 0 0.10000E+01 -0.37380E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01744 0.84159 0.12873 0.12873 v Velocity[Y] -1.6974e-18 1.8598e-17 4.002e-19 4.002e-19 v Velocity[Z] -3.9237e-18 5.0934e-18 -5.1626e-22 -5.1626e-22 v ǁVelocityǁ 0.01744 0.84159 0.12873 0.12873 v Pressure 0 0 0 0 v CourantNb 0 2.8406e-16 1.7069e-17 1.7069e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.111000000E+02 TIME STEP NUMBER 111 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14968E-11 0.12586E+00 Friction velocity uk : 0.14968E-11 0.12586E+00 Dimensionless distance yplus : 0.74838E-09 0.12586E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37095E-02 1567 0.89786E-08 0.22862E-04 0.26409E+00 c Velocity[X] 0.22862E-04 c Velocity[Y] 0.48942E-38 c Velocity[Z] 0.14860E-38 c Pressure 0.37462E-18 0 0.10000E+01 -0.37462E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017355 0.84234 0.12887 0.12887 v Velocity[Y] -1.7056e-18 1.8579e-17 4.0086e-19 4.0086e-19 v Velocity[Z] -3.9284e-18 5.092e-18 -6.9126e-22 -6.9126e-22 v ǁVelocityǁ 0.017355 0.84234 0.12887 0.12887 v Pressure 0 0 0 0 v CourantNb 0 2.8485e-16 1.7096e-17 1.7096e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.112000000E+02 TIME STEP NUMBER 112 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15267E-11 0.12556E+00 Friction velocity uk : 0.15267E-11 0.12556E+00 Dimensionless distance yplus : 0.76334E-09 0.12556E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37157E-02 1566 0.89791E-08 0.22544E-04 0.26180E+00 c Velocity[X] 0.22544E-04 c Velocity[Y] 0.47202E-38 c Velocity[Z] 0.13773E-38 c Pressure 0.37551E-18 0 0.10000E+01 -0.37551E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017271 0.84309 0.129 0.129 v Velocity[Y] -1.7141e-18 1.8561e-17 4.0149e-19 4.0149e-19 v Velocity[Z] -3.9279e-18 5.1022e-18 -8.5334e-22 -8.5334e-22 v ǁVelocityǁ 0.017271 0.84309 0.129 0.129 v Pressure 0 0 0 0 v CourantNb 0 2.8723e-16 1.713e-17 1.713e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.113000000E+02 TIME STEP NUMBER 113 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15252E-11 0.12527E+00 Friction velocity uk : 0.15252E-11 0.12527E+00 Dimensionless distance yplus : 0.76261E-09 0.12527E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37218E-02 1565 0.89801E-08 0.22234E-04 0.25955E+00 c Velocity[X] 0.22234E-04 c Velocity[Y] 0.48377E-38 c Velocity[Z] 0.13867E-38 c Pressure 0.37642E-18 0 0.10000E+01 -0.37642E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017189 0.84382 0.12913 0.12913 v Velocity[Y] -1.7225e-18 1.854e-17 4.0209e-19 4.0209e-19 v Velocity[Z] -3.9517e-18 5.0856e-18 -9.4003e-22 -9.4003e-22 v ǁVelocityǁ 0.017189 0.84382 0.12913 0.12913 v Pressure 0 0 0 0 v CourantNb 0 2.8728e-16 1.7161e-17 1.7161e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.114000000E+02 TIME STEP NUMBER 114 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15051E-11 0.12497E+00 Friction velocity uk : 0.15051E-11 0.12497E+00 Dimensionless distance yplus : 0.75255E-09 0.12497E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37279E-02 1564 0.89818E-08 0.21930E-04 0.25734E+00 c Velocity[X] 0.21930E-04 c Velocity[Y] 0.46461E-38 c Velocity[Z] 0.26771E-38 c Pressure 0.37732E-18 0 0.10000E+01 -0.37732E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017108 0.84454 0.12927 0.12927 v Velocity[Y] -1.7314e-18 1.8519e-17 4.0266e-19 4.0266e-19 v Velocity[Z] -3.9396e-18 5.1318e-18 -6.7127e-22 -6.7127e-22 v ǁVelocityǁ 0.017108 0.84454 0.12927 0.12927 v Pressure 0 0 0 0 v CourantNb 0 2.8772e-16 1.7178e-17 1.7178e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.115000000E+02 TIME STEP NUMBER 115 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15329E-11 0.12468E+00 Friction velocity uk : 0.15329E-11 0.12468E+00 Dimensionless distance yplus : 0.76647E-09 0.12468E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37339E-02 1563 0.89839E-08 0.21633E-04 0.25516E+00 c Velocity[X] 0.21633E-04 c Velocity[Y] 0.46976E-38 c Velocity[Z] 0.17896E-38 c Pressure 0.37812E-18 0 0.10000E+01 -0.37812E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.017028 0.84526 0.1294 0.1294 v Velocity[Y] -1.7398e-18 1.8499e-17 4.032e-19 4.032e-19 v Velocity[Z] -3.9281e-18 5.136e-18 -2.3146e-22 -2.3146e-22 v ǁVelocityǁ 0.017028 0.84526 0.1294 0.1294 v Pressure 0 0 0 0 v CourantNb 0 2.8782e-16 1.7207e-17 1.7207e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.116000000E+02 TIME STEP NUMBER 116 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15100E-11 0.12440E+00 Friction velocity uk : 0.15100E-11 0.12440E+00 Dimensionless distance yplus : 0.75498E-09 0.12440E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37399E-02 1562 0.89867E-08 0.21343E-04 0.25303E+00 c Velocity[X] 0.21343E-04 c Velocity[Y] 0.47738E-38 c Velocity[Z] 0.21352E-38 c Pressure 0.37904E-18 0 0.10000E+01 -0.37904E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016949 0.84596 0.12953 0.12953 v Velocity[Y] -1.7488e-18 1.8476e-17 4.0371e-19 4.0371e-19 v Velocity[Z] -3.9545e-18 5.1303e-18 -9.7557e-22 -9.7557e-22 v ǁVelocityǁ 0.016949 0.84596 0.12953 0.12953 v Pressure 0 0 0 0 v CourantNb 0 2.873e-16 1.7219e-17 1.7219e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.117000000E+02 TIME STEP NUMBER 117 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15289E-11 0.12411E+00 Friction velocity uk : 0.15289E-11 0.12411E+00 Dimensionless distance yplus : 0.76447E-09 0.12411E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37459E-02 1561 0.89900E-08 0.21060E-04 0.25093E+00 c Velocity[X] 0.21060E-04 c Velocity[Y] 0.51776E-38 c Velocity[Z] 0.17721E-38 c Pressure 0.37981E-18 0 0.10000E+01 -0.37981E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016871 0.84665 0.12966 0.12966 v Velocity[Y] -1.7587e-18 1.845e-17 4.0419e-19 4.0419e-19 v Velocity[Z] -3.9636e-18 5.1393e-18 -7.03e-22 -7.03e-22 v ǁVelocityǁ 0.016871 0.84665 0.12966 0.12966 v Pressure 0 0 0 0 v CourantNb 0 2.8783e-16 1.7256e-17 1.7256e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.118000000E+02 TIME STEP NUMBER 118 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15727E-11 0.12383E+00 Friction velocity uk : 0.15727E-11 0.12383E+00 Dimensionless distance yplus : 0.78634E-09 0.12383E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37518E-02 1560 0.89939E-08 0.20782E-04 0.24886E+00 c Velocity[X] 0.20782E-04 c Velocity[Y] 0.46112E-38 c Velocity[Z] 0.12848E-38 c Pressure 0.38067E-18 0 0.10000E+01 -0.38067E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016795 0.84733 0.12979 0.12979 v Velocity[Y] -1.768e-18 1.8427e-17 4.0463e-19 4.0463e-19 v Velocity[Z] -3.9616e-18 5.1342e-18 -7.8795e-22 -7.8795e-22 v ǁVelocityǁ 0.016795 0.84733 0.12979 0.12979 v Pressure 0 0 0 0 v CourantNb 0 2.8962e-16 1.7283e-17 1.7283e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.119000000E+02 TIME STEP NUMBER 119 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15762E-11 0.12356E+00 Friction velocity uk : 0.15762E-11 0.12356E+00 Dimensionless distance yplus : 0.78810E-09 0.12356E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37577E-02 1559 0.89982E-08 0.20510E-04 0.24683E+00 c Velocity[X] 0.20510E-04 c Velocity[Y] 0.42221E-38 c Velocity[Z] 0.14928E-38 c Pressure 0.38164E-18 0 0.10000E+01 -0.38164E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016719 0.84801 0.12992 0.12992 v Velocity[Y] -1.7777e-18 1.8403e-17 4.0505e-19 4.0505e-19 v Velocity[Z] -3.9847e-18 5.1521e-18 -1.0521e-21 -1.0521e-21 v ǁVelocityǁ 0.016719 0.84801 0.12992 0.12992 v Pressure 0 0 0 0 v CourantNb 0 2.891e-16 1.731e-17 1.731e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.120000000E+02 TIME STEP NUMBER 120 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15668E-11 0.12328E+00 Friction velocity uk : 0.15668E-11 0.12328E+00 Dimensionless distance yplus : 0.78342E-09 0.12328E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37635E-02 1558 0.90031E-08 0.20245E-04 0.24484E+00 c Velocity[X] 0.20245E-04 c Velocity[Y] 0.38839E-38 c Velocity[Z] 0.12880E-38 c Pressure 0.38248E-18 0 0.10000E+01 -0.38248E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016644 0.84867 0.13005 0.13005 v Velocity[Y] -1.7873e-18 1.8384e-17 4.0544e-19 4.0544e-19 v Velocity[Z] -3.9974e-18 5.156e-18 -1.2031e-21 -1.2031e-21 v ǁVelocityǁ 0.016644 0.84867 0.13005 0.13005 v Pressure 0 0 0 0 v CourantNb 0 2.9058e-16 1.7337e-17 1.7337e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.121000000E+02 TIME STEP NUMBER 121 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15853E-11 0.12301E+00 Friction velocity uk : 0.15853E-11 0.12301E+00 Dimensionless distance yplus : 0.79264E-09 0.12301E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37693E-02 1557 0.90086E-08 0.19985E-04 0.24287E+00 c Velocity[X] 0.19985E-04 c Velocity[Y] 0.44317E-38 c Velocity[Z] 0.16806E-38 c Pressure 0.38333E-18 0 0.10000E+01 -0.38333E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016571 0.84933 0.13018 0.13018 v Velocity[Y] -1.7966e-18 1.8361e-17 4.0581e-19 4.0581e-19 v Velocity[Z] -3.9842e-18 5.1928e-18 -7.7782e-22 -7.7782e-22 v ǁVelocityǁ 0.016571 0.84933 0.13018 0.13018 v Pressure 0 0 0 0 v CourantNb 0 2.9174e-16 1.7369e-17 1.7369e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.122000000E+02 TIME STEP NUMBER 122 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15511E-11 0.12275E+00 Friction velocity uk : 0.15511E-11 0.12275E+00 Dimensionless distance yplus : 0.77557E-09 0.12275E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37751E-02 1556 0.90145E-08 0.19730E-04 0.24094E+00 c Velocity[X] 0.19730E-04 c Velocity[Y] 0.38661E-38 c Velocity[Z] 0.12043E-38 c Pressure 0.38406E-18 0 0.10000E+01 -0.38406E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016498 0.84998 0.13031 0.13031 v Velocity[Y] -1.8061e-18 1.8338e-17 4.0615e-19 4.0615e-19 v Velocity[Z] -3.9963e-18 5.1834e-18 -7.9108e-22 -7.9108e-22 v ǁVelocityǁ 0.016498 0.84998 0.13031 0.13031 v Pressure 0 0 0 0 v CourantNb 0 2.9158e-16 1.7391e-17 1.7391e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.123000000E+02 TIME STEP NUMBER 123 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15104E-11 0.12248E+00 Friction velocity uk : 0.15104E-11 0.12248E+00 Dimensionless distance yplus : 0.75522E-09 0.12248E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37808E-02 1555 0.90210E-08 0.19481E-04 0.23904E+00 c Velocity[X] 0.19481E-04 c Velocity[Y] 0.41972E-38 c Velocity[Z] 0.16573E-38 c Pressure 0.38501E-18 0 0.10000E+01 -0.38501E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016426 0.85062 0.13044 0.13044 v Velocity[Y] -1.8155e-18 1.8314e-17 4.0646e-19 4.0646e-19 v Velocity[Z] -4.0173e-18 5.1998e-18 -6.7243e-22 -6.7243e-22 v ǁVelocityǁ 0.016426 0.85062 0.13044 0.13044 v Pressure 0 0 0 0 v CourantNb 0 2.9071e-16 1.7415e-17 1.7415e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.124000000E+02 TIME STEP NUMBER 124 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14902E-11 0.12222E+00 Friction velocity uk : 0.14902E-11 0.12222E+00 Dimensionless distance yplus : 0.74510E-09 0.12222E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37865E-02 1554 0.90279E-08 0.19237E-04 0.23717E+00 c Velocity[X] 0.19237E-04 c Velocity[Y] 0.34428E-38 c Velocity[Z] 0.15355E-38 c Pressure 0.38569E-18 0 0.10000E+01 -0.38569E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016355 0.85125 0.13056 0.13056 v Velocity[Y] -1.8258e-18 1.8293e-17 4.0675e-19 4.0675e-19 v Velocity[Z] -4.0139e-18 5.1791e-18 -9.1518e-22 -9.1518e-22 v ǁVelocityǁ 0.016355 0.85125 0.13056 0.13056 v Pressure 0 0 0 0 v CourantNb 0 2.9178e-16 1.7449e-17 1.7449e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.125000000E+02 TIME STEP NUMBER 125 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15529E-11 0.12196E+00 Friction velocity uk : 0.15529E-11 0.12196E+00 Dimensionless distance yplus : 0.77647E-09 0.12196E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37922E-02 1554 0.89631E-08 0.18998E-04 0.23533E+00 c Velocity[X] 0.18998E-04 c Velocity[Y] 0.41990E-38 c Velocity[Z] 0.14322E-38 c Pressure 0.38649E-18 0 0.10000E+01 -0.38649E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016286 0.85187 0.13069 0.13069 v Velocity[Y] -1.8358e-18 1.8268e-17 4.0701e-19 4.0701e-19 v Velocity[Z] -4.019e-18 5.1904e-18 -1.1633e-21 -1.1633e-21 v ǁVelocityǁ 0.016286 0.85187 0.13069 0.13069 v Pressure 0 0 0 0 v CourantNb 0 2.9162e-16 1.7471e-17 1.7471e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.126000000E+02 TIME STEP NUMBER 126 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15237E-11 0.12171E+00 Friction velocity uk : 0.15237E-11 0.12171E+00 Dimensionless distance yplus : 0.76183E-09 0.12171E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.37978E-02 1553 0.89710E-08 0.18764E-04 0.23352E+00 c Velocity[X] 0.18764E-04 c Velocity[Y] 0.39395E-38 c Velocity[Z] 0.12880E-38 c Pressure 0.38741E-18 0 0.10000E+01 -0.38741E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016216 0.85249 0.13082 0.13082 v Velocity[Y] -1.8463e-18 1.8244e-17 4.0725e-19 4.0725e-19 v Velocity[Z] -4.0156e-18 5.2044e-18 -9.8886e-22 -9.8886e-22 v ǁVelocityǁ 0.016216 0.85249 0.13082 0.13082 v Pressure 0 0 0 0 v CourantNb 0 2.9342e-16 1.7495e-17 1.7495e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.127000000E+02 TIME STEP NUMBER 127 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15544E-11 0.12145E+00 Friction velocity uk : 0.15544E-11 0.12145E+00 Dimensionless distance yplus : 0.77718E-09 0.12145E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38034E-02 1552 0.89793E-08 0.18534E-04 0.23173E+00 c Velocity[X] 0.18534E-04 c Velocity[Y] 0.37124E-38 c Velocity[Z] 0.21600E-38 c Pressure 0.38811E-18 0 0.10000E+01 -0.38811E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016148 0.85309 0.13094 0.13094 v Velocity[Y] -1.8578e-18 1.8221e-17 4.0746e-19 4.0746e-19 v Velocity[Z] -4.0162e-18 5.2362e-18 -1.1463e-21 -1.1463e-21 v ǁVelocityǁ 0.016148 0.85309 0.13094 0.13094 v Pressure 0 0 0 0 v CourantNb 0 2.9236e-16 1.752e-17 1.752e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.128000000E+02 TIME STEP NUMBER 128 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15350E-11 0.12120E+00 Friction velocity uk : 0.15350E-11 0.12120E+00 Dimensionless distance yplus : 0.76749E-09 0.12120E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38089E-02 1551 0.89881E-08 0.18309E-04 0.22998E+00 c Velocity[X] 0.18309E-04 c Velocity[Y] 0.39340E-38 c Velocity[Z] 0.18571E-38 c Pressure 0.38876E-18 0 0.10000E+01 -0.38876E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016081 0.85369 0.13107 0.13107 v Velocity[Y] -1.8693e-18 1.8196e-17 4.0765e-19 4.0765e-19 v Velocity[Z] -4.0192e-18 5.2135e-18 -9.864e-22 -9.864e-22 v ǁVelocityǁ 0.016081 0.85369 0.13107 0.13107 v Pressure 0 0 0 0 v CourantNb 0 2.9352e-16 1.756e-17 1.756e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.129000000E+02 TIME STEP NUMBER 129 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15231E-11 0.12096E+00 Friction velocity uk : 0.15231E-11 0.12096E+00 Dimensionless distance yplus : 0.76155E-09 0.12096E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38145E-02 1550 0.89974E-08 0.18089E-04 0.22825E+00 c Velocity[X] 0.18089E-04 c Velocity[Y] 0.38348E-38 c Velocity[Z] 0.26162E-38 c Pressure 0.38971E-18 0 0.10000E+01 -0.38971E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.016014 0.85429 0.13119 0.13119 v Velocity[Y] -1.8813e-18 1.8168e-17 4.0781e-19 4.0781e-19 v Velocity[Z] -4.0344e-18 5.219e-18 -1.0705e-21 -1.0705e-21 v ǁVelocityǁ 0.016014 0.85429 0.13119 0.13119 v Pressure 0 0 0 0 v CourantNb 0 2.9352e-16 1.7577e-17 1.7577e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.130000000E+02 TIME STEP NUMBER 130 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15312E-11 0.12071E+00 Friction velocity uk : 0.15312E-11 0.12071E+00 Dimensionless distance yplus : 0.76559E-09 0.12071E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38200E-02 1549 0.90071E-08 0.17873E-04 0.22655E+00 c Velocity[X] 0.17873E-04 c Velocity[Y] 0.29162E-38 c Velocity[Z] 0.31113E-38 c Pressure 0.39059E-18 0 0.10000E+01 -0.39059E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015949 0.85487 0.13132 0.13132 v Velocity[Y] -1.8926e-18 1.8149e-17 4.0796e-19 4.0796e-19 v Velocity[Z] -4.0286e-18 5.2676e-18 -5.4945e-22 -5.4945e-22 v ǁVelocityǁ 0.015949 0.85487 0.13132 0.13132 v Pressure 0 0 0 0 v CourantNb 0 2.9485e-16 1.7606e-17 1.7606e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.131000000E+02 TIME STEP NUMBER 131 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15351E-11 0.12047E+00 Friction velocity uk : 0.15351E-11 0.12047E+00 Dimensionless distance yplus : 0.76754E-09 0.12047E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38254E-02 1548 0.90173E-08 0.17661E-04 0.22487E+00 c Velocity[X] 0.17661E-04 c Velocity[Y] 0.28127E-38 c Velocity[Z] 0.18884E-38 c Pressure 0.39132E-18 0 0.10000E+01 -0.39132E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015884 0.85545 0.13144 0.13144 v Velocity[Y] -1.9036e-18 1.813e-17 4.0809e-19 4.0809e-19 v Velocity[Z] -4.0234e-18 5.2875e-18 -2.2906e-22 -2.2906e-22 v ǁVelocityǁ 0.015884 0.85545 0.13144 0.13144 v Pressure 0 0 0 0 v CourantNb 0 2.9538e-16 1.7645e-17 1.7645e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.132000000E+02 TIME STEP NUMBER 132 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15198E-11 0.12023E+00 Friction velocity uk : 0.15198E-11 0.12023E+00 Dimensionless distance yplus : 0.75988E-09 0.12023E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38308E-02 1547 0.90280E-08 0.17454E-04 0.22322E+00 c Velocity[X] 0.17454E-04 c Velocity[Y] 0.27357E-38 c Velocity[Z] 0.14696E-38 c Pressure 0.39209E-18 0 0.10000E+01 -0.39209E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01582 0.85602 0.13156 0.13156 v Velocity[Y] -1.9154e-18 1.8109e-17 4.082e-19 4.082e-19 v Velocity[Z] -4.0293e-18 5.2813e-18 -1.5394e-22 -1.5394e-22 v ǁVelocityǁ 0.01582 0.85602 0.13156 0.13156 v Pressure 0 0 0 0 v CourantNb 0 2.9563e-16 1.7681e-17 1.7681e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.133000000E+02 TIME STEP NUMBER 133 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15321E-11 0.11999E+00 Friction velocity uk : 0.15321E-11 0.11999E+00 Dimensionless distance yplus : 0.76607E-09 0.11999E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38362E-02 1547 0.89668E-08 0.17250E-04 0.22159E+00 c Velocity[X] 0.17250E-04 c Velocity[Y] 0.30095E-38 c Velocity[Z] 0.16711E-38 c Pressure 0.39297E-18 0 0.10000E+01 -0.39297E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015756 0.85658 0.13169 0.13169 v Velocity[Y] -1.9269e-18 1.8086e-17 4.083e-19 4.083e-19 v Velocity[Z] -4.0355e-18 5.3015e-18 -3.6486e-22 -3.6486e-22 v ǁVelocityǁ 0.015756 0.85658 0.13169 0.13169 v Pressure 0 0 0 0 v CourantNb 0 2.9511e-16 1.7689e-17 1.7689e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.134000000E+02 TIME STEP NUMBER 134 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14675E-11 0.11976E+00 Friction velocity uk : 0.14675E-11 0.11976E+00 Dimensionless distance yplus : 0.73374E-09 0.11976E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38416E-02 1546 0.89782E-08 0.17051E-04 0.21999E+00 c Velocity[X] 0.17051E-04 c Velocity[Y] 0.29323E-38 c Velocity[Z] 0.10231E-38 c Pressure 0.39373E-18 0 0.10000E+01 -0.39373E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015694 0.85714 0.13181 0.13181 v Velocity[Y] -1.9399e-18 1.8063e-17 4.0837e-19 4.0837e-19 v Velocity[Z] -4.0465e-18 5.2994e-18 -5.7503e-22 -5.7503e-22 v ǁVelocityǁ 0.015694 0.85714 0.13181 0.13181 v Pressure 0 0 0 0 v CourantNb 0 2.9561e-16 1.7729e-17 1.7729e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.135000000E+02 TIME STEP NUMBER 135 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14645E-11 0.11952E+00 Friction velocity uk : 0.14645E-11 0.11952E+00 Dimensionless distance yplus : 0.73224E-09 0.11952E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38469E-02 1545 0.89901E-08 0.16855E-04 0.21841E+00 c Velocity[X] 0.16855E-04 c Velocity[Y] 0.31566E-38 c Velocity[Z] 0.15060E-38 c Pressure 0.39448E-18 0 0.10000E+01 -0.39448E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015632 0.85769 0.13193 0.13193 v Velocity[Y] -1.9517e-18 1.8039e-17 4.0843e-19 4.0843e-19 v Velocity[Z] -4.0369e-18 5.301e-18 -2.544e-22 -2.544e-22 v ǁVelocityǁ 0.015632 0.85769 0.13193 0.13193 v Pressure 0 0 0 0 v CourantNb 0 2.9645e-16 1.774e-17 1.774e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.136000000E+02 TIME STEP NUMBER 136 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15456E-11 0.11929E+00 Friction velocity uk : 0.15456E-11 0.11929E+00 Dimensionless distance yplus : 0.77281E-09 0.11929E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38522E-02 1544 0.90024E-08 0.16662E-04 0.21685E+00 c Velocity[X] 0.16662E-04 c Velocity[Y] 0.25669E-38 c Velocity[Z] 0.13302E-38 c Pressure 0.39514E-18 0 0.10000E+01 -0.39514E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015571 0.85823 0.13205 0.13205 v Velocity[Y] -1.9636e-18 1.8016e-17 4.0847e-19 4.0847e-19 v Velocity[Z] -4.0466e-18 5.3033e-18 -6.7745e-22 -6.7745e-22 v ǁVelocityǁ 0.015571 0.85823 0.13205 0.13205 v Pressure 0 0 0 0 v CourantNb 0 2.9596e-16 1.7753e-17 1.7753e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.137000000E+02 TIME STEP NUMBER 137 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15852E-11 0.11907E+00 Friction velocity uk : 0.15852E-11 0.11907E+00 Dimensionless distance yplus : 0.79261E-09 0.11907E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38575E-02 1543 0.90151E-08 0.16474E-04 0.21531E+00 c Velocity[X] 0.16474E-04 c Velocity[Y] 0.30178E-38 c Velocity[Z] 0.12219E-38 c Pressure 0.39593E-18 0 0.10000E+01 -0.39593E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01551 0.85877 0.13217 0.13217 v Velocity[Y] -1.9748e-18 1.7991e-17 4.0849e-19 4.0849e-19 v Velocity[Z] -4.0623e-18 5.3165e-18 -5.8339e-22 -5.8339e-22 v ǁVelocityǁ 0.01551 0.85877 0.13217 0.13217 v Pressure 0 0 0 0 v CourantNb 0 2.9641e-16 1.7762e-17 1.7762e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.138000000E+02 TIME STEP NUMBER 138 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15601E-11 0.11884E+00 Friction velocity uk : 0.15601E-11 0.11884E+00 Dimensionless distance yplus : 0.78005E-09 0.11884E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38628E-02 1542 0.90282E-08 0.16289E-04 0.21380E+00 c Velocity[X] 0.16289E-04 c Velocity[Y] 0.28055E-38 c Velocity[Z] 0.12062E-38 c Pressure 0.39659E-18 0 0.10000E+01 -0.39659E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015451 0.8593 0.13229 0.13229 v Velocity[Y] -1.9853e-18 1.7966e-17 4.0849e-19 4.0849e-19 v Velocity[Z] -4.0696e-18 5.2977e-18 -7.9387e-22 -7.9387e-22 v ǁVelocityǁ 0.015451 0.8593 0.13229 0.13229 v Pressure 0 0 0 0 v CourantNb 0 2.9696e-16 1.7799e-17 1.7799e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.139000000E+02 TIME STEP NUMBER 139 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15766E-11 0.11862E+00 Friction velocity uk : 0.15766E-11 0.11862E+00 Dimensionless distance yplus : 0.78829E-09 0.11862E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38680E-02 1542 0.89695E-08 0.16107E-04 0.21231E+00 c Velocity[X] 0.16107E-04 c Velocity[Y] 0.30061E-38 c Velocity[Z] 0.20687E-38 c Pressure 0.39744E-18 0 0.10000E+01 -0.39744E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015392 0.85983 0.13241 0.13241 v Velocity[Y] -1.9983e-18 1.7944e-17 4.0848e-19 4.0848e-19 v Velocity[Z] -4.0688e-18 5.3332e-18 -7.67e-22 -7.67e-22 v ǁVelocityǁ 0.015392 0.85983 0.13241 0.13241 v Pressure 0 0 0 0 v CourantNb 0 2.9772e-16 1.7802e-17 1.7802e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.140000000E+02 TIME STEP NUMBER 140 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16416E-11 0.11839E+00 Friction velocity uk : 0.16416E-11 0.11839E+00 Dimensionless distance yplus : 0.82079E-09 0.11839E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38732E-02 1541 0.89834E-08 0.15929E-04 0.21084E+00 c Velocity[X] 0.15929E-04 c Velocity[Y] 0.33104E-38 c Velocity[Z] 0.16057E-38 c Pressure 0.39809E-18 0 0.10000E+01 -0.39809E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015333 0.86035 0.13253 0.13253 v Velocity[Y] -2.0101e-18 1.7916e-17 4.0844e-19 4.0844e-19 v Velocity[Z] -4.106e-18 5.3312e-18 -6.9188e-22 -6.9188e-22 v ǁVelocityǁ 0.015333 0.86035 0.13253 0.13253 v Pressure 0 0 0 0 v CourantNb 0 2.9713e-16 1.7852e-17 1.7852e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.141000000E+02 TIME STEP NUMBER 141 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16671E-11 0.11817E+00 Friction velocity uk : 0.16671E-11 0.11817E+00 Dimensionless distance yplus : 0.83355E-09 0.11817E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38783E-02 1540 0.89977E-08 0.15754E-04 0.20939E+00 c Velocity[X] 0.15754E-04 c Velocity[Y] 0.25185E-38 c Velocity[Z] 0.27206E-38 c Pressure 0.39901E-18 0 0.10000E+01 -0.39901E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015275 0.86086 0.13265 0.13265 v Velocity[Y] -2.0232e-18 1.7896e-17 4.0839e-19 4.0839e-19 v Velocity[Z] -4.0873e-18 5.3509e-18 -5.0374e-22 -5.0374e-22 v ǁVelocityǁ 0.015275 0.86086 0.13265 0.13265 v Pressure 0 0 0 0 v CourantNb 0 2.9747e-16 1.7859e-17 1.7859e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.142000000E+02 TIME STEP NUMBER 142 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16786E-11 0.11796E+00 Friction velocity uk : 0.16786E-11 0.11796E+00 Dimensionless distance yplus : 0.83928E-09 0.11796E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38835E-02 1539 0.90123E-08 0.15582E-04 0.20796E+00 c Velocity[X] 0.15582E-04 c Velocity[Y] 0.26548E-38 c Velocity[Z] 0.15304E-38 c Pressure 0.39973E-18 0 0.10000E+01 -0.39973E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015218 0.86137 0.13276 0.13276 v Velocity[Y] -2.0358e-18 1.7874e-17 4.0831e-19 4.0831e-19 v Velocity[Z] -4.0927e-18 5.3398e-18 -7.8372e-22 -7.8372e-22 v ǁVelocityǁ 0.015218 0.86137 0.13276 0.13276 v Pressure 0 0 0 0 v CourantNb 0 2.9835e-16 1.7902e-17 1.7902e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.143000000E+02 TIME STEP NUMBER 143 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17210E-11 0.11774E+00 Friction velocity uk : 0.17210E-11 0.11774E+00 Dimensionless distance yplus : 0.86049E-09 0.11774E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38886E-02 1538 0.90274E-08 0.15413E-04 0.20655E+00 c Velocity[X] 0.15413E-04 c Velocity[Y] 0.24203E-38 c Velocity[Z] 0.16529E-38 c Pressure 0.40036E-18 0 0.10000E+01 -0.40036E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015162 0.86187 0.13288 0.13288 v Velocity[Y] -2.0483e-18 1.7852e-17 4.0823e-19 4.0823e-19 v Velocity[Z] -4.0777e-18 5.348e-18 -8.4882e-22 -8.4882e-22 v ǁVelocityǁ 0.015162 0.86187 0.13288 0.13288 v Pressure 0 0 0 0 v CourantNb 0 2.9917e-16 1.792e-17 1.792e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.144000000E+02 TIME STEP NUMBER 144 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18336E-11 0.11753E+00 Friction velocity uk : 0.18336E-11 0.11753E+00 Dimensionless distance yplus : 0.91682E-09 0.11753E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38936E-02 1538 0.89706E-08 0.15247E-04 0.20516E+00 c Velocity[X] 0.15247E-04 c Velocity[Y] 0.25593E-38 c Velocity[Z] 0.18125E-38 c Pressure 0.40123E-18 0 0.10000E+01 -0.40123E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015106 0.86237 0.133 0.133 v Velocity[Y] -2.0605e-18 1.7829e-17 4.0813e-19 4.0813e-19 v Velocity[Z] -4.1066e-18 5.3614e-18 -9.2045e-22 -9.2045e-22 v ǁVelocityǁ 0.015106 0.86237 0.133 0.133 v Pressure 0 0 0 0 v CourantNb 0 3.0032e-16 1.7951e-17 1.7951e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.145000000E+02 TIME STEP NUMBER 145 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16757E-11 0.11732E+00 Friction velocity uk : 0.16757E-11 0.11732E+00 Dimensionless distance yplus : 0.83786E-09 0.11732E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.38987E-02 1537 0.89864E-08 0.15084E-04 0.20379E+00 c Velocity[X] 0.15084E-04 c Velocity[Y] 0.25127E-38 c Velocity[Z] 0.10205E-38 c Pressure 0.40186E-18 0 0.10000E+01 -0.40186E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.015051 0.86286 0.13312 0.13312 v Velocity[Y] -2.0729e-18 1.7806e-17 4.0801e-19 4.0801e-19 v Velocity[Z] -4.1012e-18 5.3646e-18 -8.0591e-22 -8.0591e-22 v ǁVelocityǁ 0.015051 0.86286 0.13312 0.13312 v Pressure 0 0 0 0 v CourantNb 0 2.9936e-16 1.7985e-17 1.7985e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.146000000E+02 TIME STEP NUMBER 146 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15930E-11 0.11711E+00 Friction velocity uk : 0.15930E-11 0.11711E+00 Dimensionless distance yplus : 0.79649E-09 0.11711E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39037E-02 1536 0.90025E-08 0.14924E-04 0.20243E+00 c Velocity[X] 0.14924E-04 c Velocity[Y] 0.24206E-38 c Velocity[Z] 0.12390E-38 c Pressure 0.40256E-18 0 0.10000E+01 -0.40256E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014996 0.86335 0.13323 0.13323 v Velocity[Y] -2.0857e-18 1.7783e-17 4.0787e-19 4.0787e-19 v Velocity[Z] -4.1178e-18 5.3675e-18 -6.7113e-22 -6.7113e-22 v ǁVelocityǁ 0.014996 0.86335 0.13323 0.13323 v Pressure 0 0 0 0 v CourantNb 0 3.0015e-16 1.8002e-17 1.8002e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.147000000E+02 TIME STEP NUMBER 147 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15330E-11 0.11690E+00 Friction velocity uk : 0.15330E-11 0.11690E+00 Dimensionless distance yplus : 0.76651E-09 0.11690E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39087E-02 1535 0.90190E-08 0.14767E-04 0.20110E+00 c Velocity[X] 0.14767E-04 c Velocity[Y] 0.23559E-38 c Velocity[Z] 0.16613E-38 c Pressure 0.40343E-18 0 0.10000E+01 -0.40343E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014942 0.86383 0.13335 0.13335 v Velocity[Y] -2.099e-18 1.7762e-17 4.0772e-19 4.0772e-19 v Velocity[Z] -4.1141e-18 5.3747e-18 -5.2861e-22 -5.2861e-22 v ǁVelocityǁ 0.014942 0.86383 0.13335 0.13335 v Pressure 0 0 0 0 v CourantNb 0 3.0108e-16 1.8022e-17 1.8022e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.148000000E+02 TIME STEP NUMBER 148 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17225E-11 0.11669E+00 Friction velocity uk : 0.17225E-11 0.11669E+00 Dimensionless distance yplus : 0.86127E-09 0.11669E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39137E-02 1534 0.90359E-08 0.14612E-04 0.19978E+00 c Velocity[X] 0.14612E-04 c Velocity[Y] 0.24559E-38 c Velocity[Z] 0.15384E-38 c Pressure 0.40417E-18 0 0.10000E+01 -0.40417E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014889 0.8643 0.13346 0.13346 v Velocity[Y] -2.1115e-18 1.7739e-17 4.0756e-19 4.0756e-19 v Velocity[Z] -4.1421e-18 5.3831e-18 -7.7396e-22 -7.7396e-22 v ǁVelocityǁ 0.014889 0.8643 0.13346 0.13346 v Pressure 0 0 0 0 v CourantNb 0 3.0023e-16 1.8049e-17 1.8049e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.149000000E+02 TIME STEP NUMBER 149 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14752E-11 0.11649E+00 Friction velocity uk : 0.14752E-11 0.11649E+00 Dimensionless distance yplus : 0.73759E-09 0.11649E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39186E-02 1534 0.89808E-08 0.14460E-04 0.19848E+00 c Velocity[X] 0.14460E-04 c Velocity[Y] 0.24197E-38 c Velocity[Z] 0.13499E-38 c Pressure 0.40479E-18 0 0.10000E+01 -0.40479E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014836 0.86477 0.13358 0.13358 v Velocity[Y] -2.125e-18 1.7714e-17 4.0738e-19 4.0738e-19 v Velocity[Z] -4.1419e-18 5.3969e-18 -7.7394e-22 -7.7394e-22 v ǁVelocityǁ 0.014836 0.86477 0.13358 0.13358 v Pressure 0 0 0 0 v CourantNb 0 3.0148e-16 1.8089e-17 1.8089e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.150000000E+02 TIME STEP NUMBER 150 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18535E-11 0.11629E+00 Friction velocity uk : 0.18535E-11 0.11629E+00 Dimensionless distance yplus : 0.92675E-09 0.11629E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39236E-02 1533 0.89983E-08 0.14311E-04 0.19720E+00 c Velocity[X] 0.14311E-04 c Velocity[Y] 0.24681E-38 c Velocity[Z] 0.13571E-38 c Pressure 0.40543E-18 0 0.10000E+01 -0.40543E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014783 0.86524 0.13369 0.13369 v Velocity[Y] -2.1379e-18 1.769e-17 4.0718e-19 4.0718e-19 v Velocity[Z] -4.1454e-18 5.3826e-18 -7.9125e-22 -7.9125e-22 v ǁVelocityǁ 0.014783 0.86524 0.13369 0.13369 v Pressure 0 0 0 0 v CourantNb 0 3.0223e-16 1.8107e-17 1.8107e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.151000000E+02 TIME STEP NUMBER 151 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16843E-11 0.11609E+00 Friction velocity uk : 0.16843E-11 0.11609E+00 Dimensionless distance yplus : 0.84217E-09 0.11609E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39285E-02 1532 0.90162E-08 0.14164E-04 0.19593E+00 c Velocity[X] 0.14164E-04 c Velocity[Y] 0.24179E-38 c Velocity[Z] 0.13791E-38 c Pressure 0.40613E-18 0 0.10000E+01 -0.40613E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014731 0.8657 0.13381 0.13381 v Velocity[Y] -2.1508e-18 1.7665e-17 4.0697e-19 4.0697e-19 v Velocity[Z] -4.1446e-18 5.3903e-18 -8.9615e-22 -8.9615e-22 v ǁVelocityǁ 0.014731 0.8657 0.13381 0.13381 v Pressure 0 0 0 0 v CourantNb 0 3.0287e-16 1.8143e-17 1.8143e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.152000000E+02 TIME STEP NUMBER 152 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17290E-11 0.11589E+00 Friction velocity uk : 0.17290E-11 0.11589E+00 Dimensionless distance yplus : 0.86448E-09 0.11589E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39333E-02 1531 0.90345E-08 0.14020E-04 0.19468E+00 c Velocity[X] 0.14020E-04 c Velocity[Y] 0.27754E-38 c Velocity[Z] 0.14676E-38 c Pressure 0.40680E-18 0 0.10000E+01 -0.40680E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01468 0.86615 0.13392 0.13392 v Velocity[Y] -2.1655e-18 1.7638e-17 4.0675e-19 4.0675e-19 v Velocity[Z] -4.1254e-18 5.3982e-18 -9.6367e-22 -9.6367e-22 v ǁVelocityǁ 0.01468 0.86615 0.13392 0.13392 v Pressure 0 0 0 0 v CourantNb 0 3.0227e-16 1.8156e-17 1.8156e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.153000000E+02 TIME STEP NUMBER 153 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17482E-11 0.11569E+00 Friction velocity uk : 0.17482E-11 0.11569E+00 Dimensionless distance yplus : 0.87409E-09 0.11569E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39382E-02 1531 0.89808E-08 0.13878E-04 0.19345E+00 c Velocity[X] 0.13878E-04 c Velocity[Y] 0.25243E-38 c Velocity[Z] 0.13970E-38 c Pressure 0.40749E-18 0 0.10000E+01 -0.40749E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014629 0.8666 0.13404 0.13404 v Velocity[Y] -2.1799e-18 1.7615e-17 4.0651e-19 4.0651e-19 v Velocity[Z] -4.1535e-18 5.3979e-18 -8.5129e-22 -8.5129e-22 v ǁVelocityǁ 0.014629 0.8666 0.13404 0.13404 v Pressure 0 0 0 0 v CourantNb 0 3.0284e-16 1.8162e-17 1.8162e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.154000000E+02 TIME STEP NUMBER 154 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17645E-11 0.11550E+00 Friction velocity uk : 0.17645E-11 0.11550E+00 Dimensionless distance yplus : 0.88223E-09 0.11550E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39430E-02 1530 0.89996E-08 0.13739E-04 0.19223E+00 c Velocity[X] 0.13739E-04 c Velocity[Y] 0.26246E-38 c Velocity[Z] 0.23917E-38 c Pressure 0.40823E-18 0 0.10000E+01 -0.40823E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014579 0.86705 0.13415 0.13415 v Velocity[Y] -2.1936e-18 1.7591e-17 4.0626e-19 4.0626e-19 v Velocity[Z] -4.1444e-18 5.4275e-18 -6.2929e-22 -6.2929e-22 v ǁVelocityǁ 0.014579 0.86705 0.13415 0.13415 v Pressure 0 0 0 0 v CourantNb 0 3.0311e-16 1.8186e-17 1.8186e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.155000000E+02 TIME STEP NUMBER 155 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16539E-11 0.11530E+00 Friction velocity uk : 0.16539E-11 0.11530E+00 Dimensionless distance yplus : 0.82695E-09 0.11530E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39478E-02 1529 0.90188E-08 0.13602E-04 0.19103E+00 c Velocity[X] 0.13602E-04 c Velocity[Y] 0.25748E-38 c Velocity[Z] 0.17086E-38 c Pressure 0.40885E-18 0 0.10000E+01 -0.40885E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014529 0.86749 0.13426 0.13426 v Velocity[Y] -2.2083e-18 1.7566e-17 4.0599e-19 4.0599e-19 v Velocity[Z] -4.1474e-18 5.4094e-18 -8.4212e-22 -8.4212e-22 v ǁVelocityǁ 0.014529 0.86749 0.13426 0.13426 v Pressure 0 0 0 0 v CourantNb 0 3.036e-16 1.8214e-17 1.8214e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.156000000E+02 TIME STEP NUMBER 156 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16921E-11 0.11511E+00 Friction velocity uk : 0.16921E-11 0.11511E+00 Dimensionless distance yplus : 0.84605E-09 0.11511E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39526E-02 1528 0.90384E-08 0.13467E-04 0.18984E+00 c Velocity[X] 0.13467E-04 c Velocity[Y] 0.25668E-38 c Velocity[Z] 0.14056E-38 c Pressure 0.40968E-18 0 0.10000E+01 -0.40968E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01448 0.86793 0.13437 0.13437 v Velocity[Y] -2.2224e-18 1.7541e-17 4.057e-19 4.057e-19 v Velocity[Z] -4.1591e-18 5.4169e-18 -7.6031e-22 -7.6031e-22 v ǁVelocityǁ 0.01448 0.86793 0.13437 0.13437 v Pressure 0 0 0 0 v CourantNb 0 3.0352e-16 1.8237e-17 1.8237e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.157000000E+02 TIME STEP NUMBER 157 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16718E-11 0.11492E+00 Friction velocity uk : 0.16718E-11 0.11492E+00 Dimensionless distance yplus : 0.83588E-09 0.11492E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39573E-02 1528 0.89859E-08 0.13334E-04 0.18867E+00 c Velocity[X] 0.13334E-04 c Velocity[Y] 0.26058E-38 c Velocity[Z] 0.97600E-39 c Pressure 0.41032E-18 0 0.10000E+01 -0.41032E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014431 0.86836 0.13448 0.13448 v Velocity[Y] -2.2366e-18 1.7515e-17 4.054e-19 4.054e-19 v Velocity[Z] -4.1498e-18 5.4321e-18 -6.6492e-22 -6.6492e-22 v ǁVelocityǁ 0.014431 0.86836 0.13448 0.13448 v Pressure 0 0 0 0 v CourantNb 0 3.0393e-16 1.8253e-17 1.8253e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.158000000E+02 TIME STEP NUMBER 158 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16429E-11 0.11473E+00 Friction velocity uk : 0.16429E-11 0.11473E+00 Dimensionless distance yplus : 0.82143E-09 0.11473E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39621E-02 1527 0.90060E-08 0.13203E-04 0.18751E+00 c Velocity[X] 0.13203E-04 c Velocity[Y] 0.24776E-38 c Velocity[Z] 0.10629E-38 c Pressure 0.41095E-18 0 0.10000E+01 -0.41095E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014383 0.86879 0.1346 0.1346 v Velocity[Y] -2.2502e-18 1.749e-17 4.0508e-19 4.0508e-19 v Velocity[Z] -4.1721e-18 5.4375e-18 -7.2132e-22 -7.2132e-22 v ǁVelocityǁ 0.014383 0.86879 0.1346 0.1346 v Pressure 0 0 0 0 v CourantNb 0 3.0341e-16 1.8275e-17 1.8275e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.159000000E+02 TIME STEP NUMBER 159 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15992E-11 0.11455E+00 Friction velocity uk : 0.15992E-11 0.11455E+00 Dimensionless distance yplus : 0.79958E-09 0.11455E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39668E-02 1526 0.90265E-08 0.13075E-04 0.18637E+00 c Velocity[X] 0.13075E-04 c Velocity[Y] 0.21864E-38 c Velocity[Z] 0.11037E-38 c Pressure 0.41164E-18 0 0.10000E+01 -0.41164E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014335 0.86922 0.13471 0.13471 v Velocity[Y] -2.2634e-18 1.7467e-17 4.0475e-19 4.0475e-19 v Velocity[Z] -4.1477e-18 5.4314e-18 -7.6043e-22 -7.6043e-22 v ǁVelocityǁ 0.014335 0.86922 0.13471 0.13471 v Pressure 0 0 0 0 v CourantNb 0 3.0418e-16 1.8299e-17 1.8299e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.160000000E+02 TIME STEP NUMBER 160 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15597E-11 0.11436E+00 Friction velocity uk : 0.15597E-11 0.11436E+00 Dimensionless distance yplus : 0.77984E-09 0.11436E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39715E-02 1526 0.89751E-08 0.12948E-04 0.18524E+00 c Velocity[X] 0.12948E-04 c Velocity[Y] 0.26423E-38 c Velocity[Z] 0.18653E-38 c Pressure 0.41235E-18 0 0.10000E+01 -0.41235E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014288 0.86964 0.13482 0.13482 v Velocity[Y] -2.2787e-18 1.7443e-17 4.0441e-19 4.0441e-19 v Velocity[Z] -4.1633e-18 5.4311e-18 -8.4211e-22 -8.4211e-22 v ǁVelocityǁ 0.014288 0.86964 0.13482 0.13482 v Pressure 0 0 0 0 v CourantNb 0 3.0469e-16 1.8311e-17 1.8311e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.161000000E+02 TIME STEP NUMBER 161 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16675E-11 0.11418E+00 Friction velocity uk : 0.16675E-11 0.11418E+00 Dimensionless distance yplus : 0.83377E-09 0.11418E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39761E-02 1525 0.89961E-08 0.12824E-04 0.18412E+00 c Velocity[X] 0.12824E-04 c Velocity[Y] 0.22304E-38 c Velocity[Z] 0.14732E-38 c Pressure 0.41307E-18 0 0.10000E+01 -0.41307E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014241 0.87005 0.13493 0.13493 v Velocity[Y] -2.2936e-18 1.7418e-17 4.0405e-19 4.0405e-19 v Velocity[Z] -4.1656e-18 5.4693e-18 -7.5374e-22 -7.5374e-22 v ǁVelocityǁ 0.014241 0.87005 0.13493 0.13493 v Pressure 0 0 0 0 v CourantNb 0 3.0527e-16 1.8361e-17 1.8361e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.162000000E+02 TIME STEP NUMBER 162 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17818E-11 0.11399E+00 Friction velocity uk : 0.17818E-11 0.11399E+00 Dimensionless distance yplus : 0.89092E-09 0.11399E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39808E-02 1524 0.90174E-08 0.12701E-04 0.18302E+00 c Velocity[X] 0.12701E-04 c Velocity[Y] 0.29925E-38 c Velocity[Z] 0.15642E-38 c Pressure 0.41362E-18 0 0.10000E+01 -0.41362E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014195 0.87046 0.13504 0.13504 v Velocity[Y] -2.3081e-18 1.7389e-17 4.0368e-19 4.0368e-19 v Velocity[Z] -4.1638e-18 5.4497e-18 -8.3864e-22 -8.3864e-22 v ǁVelocityǁ 0.014195 0.87046 0.13504 0.13504 v Pressure 0 0 0 0 v CourantNb 0 3.054e-16 1.8378e-17 1.8378e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.163000000E+02 TIME STEP NUMBER 163 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18647E-11 0.11381E+00 Friction velocity uk : 0.18647E-11 0.11381E+00 Dimensionless distance yplus : 0.93234E-09 0.11381E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39854E-02 1523 0.90391E-08 0.12581E-04 0.18193E+00 c Velocity[X] 0.12581E-04 c Velocity[Y] 0.19799E-38 c Velocity[Z] 0.17587E-38 c Pressure 0.41429E-18 0 0.10000E+01 -0.41429E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014149 0.87087 0.13515 0.13515 v Velocity[Y] -2.3219e-18 1.7367e-17 4.0329e-19 4.0329e-19 v Velocity[Z] -4.1395e-18 5.4565e-18 -3.9046e-22 -3.9046e-22 v ǁVelocityǁ 0.014149 0.87087 0.13515 0.13515 v Pressure 0 0 0 0 v CourantNb 0 3.0563e-16 1.8387e-17 1.8387e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.164000000E+02 TIME STEP NUMBER 164 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18083E-11 0.11363E+00 Friction velocity uk : 0.18083E-11 0.11363E+00 Dimensionless distance yplus : 0.90415E-09 0.11363E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39900E-02 1523 0.89887E-08 0.12462E-04 0.18086E+00 c Velocity[X] 0.12462E-04 c Velocity[Y] 0.27170E-38 c Velocity[Z] 0.19074E-38 c Pressure 0.41504E-18 0 0.10000E+01 -0.41504E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014103 0.87128 0.13526 0.13526 v Velocity[Y] -2.3365e-18 1.7343e-17 4.0289e-19 4.0289e-19 v Velocity[Z] -4.1675e-18 5.4722e-18 -7.671e-22 -7.671e-22 v ǁVelocityǁ 0.014103 0.87128 0.13526 0.13526 v Pressure 0 0 0 0 v CourantNb 0 3.0541e-16 1.8398e-17 1.8398e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.165000000E+02 TIME STEP NUMBER 165 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17084E-11 0.11346E+00 Friction velocity uk : 0.17084E-11 0.11346E+00 Dimensionless distance yplus : 0.85421E-09 0.11346E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39946E-02 1522 0.90109E-08 0.12345E-04 0.17980E+00 c Velocity[X] 0.12345E-04 c Velocity[Y] 0.22655E-38 c Velocity[Z] 0.13967E-38 c Pressure 0.41565E-18 0 0.10000E+01 -0.41565E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014058 0.87168 0.13537 0.13537 v Velocity[Y] -2.3516e-18 1.7318e-17 4.0247e-19 4.0247e-19 v Velocity[Z] -4.1633e-18 5.4824e-18 -6.1224e-22 -6.1224e-22 v ǁVelocityǁ 0.014058 0.87168 0.13537 0.13537 v Pressure 0 0 0 0 v CourantNb 0 3.0636e-16 1.8439e-17 1.8439e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.166000000E+02 TIME STEP NUMBER 166 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17927E-11 0.11328E+00 Friction velocity uk : 0.17927E-11 0.11328E+00 Dimensionless distance yplus : 0.89637E-09 0.11328E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.39992E-02 1521 0.90334E-08 0.12230E-04 0.17875E+00 c Velocity[X] 0.12230E-04 c Velocity[Y] 0.21919E-38 c Velocity[Z] 0.20124E-38 c Pressure 0.41625E-18 0 0.10000E+01 -0.41625E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.014014 0.87207 0.13547 0.13547 v Velocity[Y] -2.3668e-18 1.7294e-17 4.0204e-19 4.0204e-19 v Velocity[Z] -4.1821e-18 5.4591e-18 -1.0351e-21 -1.0351e-21 v ǁVelocityǁ 0.014014 0.87207 0.13547 0.13547 v Pressure 0 0 0 0 v CourantNb 0 3.0593e-16 1.8444e-17 1.8444e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.167000000E+02 TIME STEP NUMBER 167 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17509E-11 0.11310E+00 Friction velocity uk : 0.17509E-11 0.11310E+00 Dimensionless distance yplus : 0.87546E-09 0.11310E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40037E-02 1521 0.89840E-08 0.12117E-04 0.17771E+00 c Velocity[X] 0.12117E-04 c Velocity[Y] 0.24269E-38 c Velocity[Z] 0.17743E-38 c Pressure 0.41695E-18 0 0.10000E+01 -0.41695E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013969 0.87247 0.13558 0.13558 v Velocity[Y] -2.3818e-18 1.7269e-17 4.016e-19 4.016e-19 v Velocity[Z] -4.1783e-18 5.4783e-18 -1.0483e-21 -1.0483e-21 v ǁVelocityǁ 0.013969 0.87247 0.13558 0.13558 v Pressure 0 0 0 0 v CourantNb 0 3.0676e-16 1.8481e-17 1.8481e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.168000000E+02 TIME STEP NUMBER 168 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18593E-11 0.11293E+00 Friction velocity uk : 0.18593E-11 0.11293E+00 Dimensionless distance yplus : 0.92963E-09 0.11293E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40082E-02 1520 0.90070E-08 0.12005E-04 0.17668E+00 c Velocity[X] 0.12005E-04 c Velocity[Y] 0.18790E-38 c Velocity[Z] 0.19916E-38 c Pressure 0.41766E-18 0 0.10000E+01 -0.41766E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013926 0.87285 0.13569 0.13569 v Velocity[Y] -2.3973e-18 1.7249e-17 4.0115e-19 4.0115e-19 v Velocity[Z] -4.1601e-18 5.4876e-18 -3.7252e-22 -3.7252e-22 v ǁVelocityǁ 0.013926 0.87285 0.13569 0.13569 v Pressure 0 0 0 0 v CourantNb 0 3.0684e-16 1.8496e-17 1.8496e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.169000000E+02 TIME STEP NUMBER 169 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19961E-11 0.11276E+00 Friction velocity uk : 0.19961E-11 0.11276E+00 Dimensionless distance yplus : 0.99807E-09 0.11276E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40127E-02 1519 0.90303E-08 0.11896E-04 0.17567E+00 c Velocity[X] 0.11896E-04 c Velocity[Y] 0.18535E-38 c Velocity[Z] 0.10384E-38 c Pressure 0.41834E-18 0 0.10000E+01 -0.41834E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013882 0.87324 0.1358 0.1358 v Velocity[Y] -2.412e-18 1.7227e-17 4.0069e-19 4.0069e-19 v Velocity[Z] -4.1739e-18 5.5017e-18 -2.7001e-22 -2.7001e-22 v ǁVelocityǁ 0.013882 0.87324 0.1358 0.1358 v Pressure 0 0 0 0 v CourantNb 0 3.0647e-16 1.8515e-17 1.8515e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.170000000E+02 TIME STEP NUMBER 170 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18080E-11 0.11259E+00 Friction velocity uk : 0.18080E-11 0.11259E+00 Dimensionless distance yplus : 0.90400E-09 0.11259E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40172E-02 1519 0.89817E-08 0.11787E-04 0.17467E+00 c Velocity[X] 0.11787E-04 c Velocity[Y] 0.20304E-38 c Velocity[Z] 0.13489E-38 c Pressure 0.41897E-18 0 0.10000E+01 -0.41897E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013839 0.87362 0.1359 0.1359 v Velocity[Y] -2.4272e-18 1.7204e-17 4.0022e-19 4.0022e-19 v Velocity[Z] -4.1524e-18 5.4961e-18 -3.6286e-22 -3.6286e-22 v ǁVelocityǁ 0.013839 0.87362 0.1359 0.1359 v Pressure 0 0 0 0 v CourantNb 0 3.0671e-16 1.8534e-17 1.8534e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.171000000E+02 TIME STEP NUMBER 171 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19055E-11 0.11242E+00 Friction velocity uk : 0.19055E-11 0.11242E+00 Dimensionless distance yplus : 0.95274E-09 0.11242E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40216E-02 1518 0.90055E-08 0.11681E-04 0.17368E+00 c Velocity[X] 0.11681E-04 c Velocity[Y] 0.17737E-38 c Velocity[Z] 0.18690E-38 c Pressure 0.41971E-18 0 0.10000E+01 -0.41971E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013796 0.874 0.13601 0.13601 v Velocity[Y] -2.4428e-18 1.7184e-17 3.9975e-19 3.9975e-19 v Velocity[Z] -4.1688e-18 5.5084e-18 -4.0165e-22 -4.0165e-22 v ǁVelocityǁ 0.013796 0.874 0.13601 0.13601 v Pressure 0 0 0 0 v CourantNb 0 3.0787e-16 1.8563e-17 1.8563e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.172000000E+02 TIME STEP NUMBER 172 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17647E-11 0.11225E+00 Friction velocity uk : 0.17647E-11 0.11225E+00 Dimensionless distance yplus : 0.88236E-09 0.11225E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40261E-02 1517 0.90297E-08 0.11576E-04 0.17270E+00 c Velocity[X] 0.11576E-04 c Velocity[Y] 0.20184E-38 c Velocity[Z] 0.17693E-38 c Pressure 0.42035E-18 0 0.10000E+01 -0.42035E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013754 0.87437 0.13612 0.13612 v Velocity[Y] -2.4584e-18 1.7161e-17 3.9926e-19 3.9926e-19 v Velocity[Z] -4.1952e-18 5.5274e-18 -8.0379e-22 -8.0379e-22 v ǁVelocityǁ 0.013754 0.87437 0.13612 0.13612 v Pressure 0 0 0 0 v CourantNb 0 3.0757e-16 1.8586e-17 1.8586e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.173000000E+02 TIME STEP NUMBER 173 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16146E-11 0.11208E+00 Friction velocity uk : 0.16146E-11 0.11208E+00 Dimensionless distance yplus : 0.80728E-09 0.11208E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40305E-02 1517 0.89818E-08 0.11472E-04 0.17173E+00 c Velocity[X] 0.11472E-04 c Velocity[Y] 0.18930E-38 c Velocity[Z] 0.16475E-38 c Pressure 0.42110E-18 0 0.10000E+01 -0.42110E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013712 0.87475 0.13622 0.13622 v Velocity[Y] -2.4738e-18 1.714e-17 3.9876e-19 3.9876e-19 v Velocity[Z] -4.1797e-18 5.5315e-18 -5.9008e-22 -5.9008e-22 v ǁVelocityǁ 0.013712 0.87475 0.13622 0.13622 v Pressure 0 0 0 0 v CourantNb 0 3.0852e-16 1.8617e-17 1.8617e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.174000000E+02 TIME STEP NUMBER 174 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17021E-11 0.11192E+00 Friction velocity uk : 0.17021E-11 0.11192E+00 Dimensionless distance yplus : 0.85104E-09 0.11192E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40349E-02 1516 0.90064E-08 0.11370E-04 0.17077E+00 c Velocity[X] 0.11370E-04 c Velocity[Y] 0.24299E-38 c Velocity[Z] 0.12282E-38 c Pressure 0.42163E-18 0 0.10000E+01 -0.42163E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013671 0.87511 0.13633 0.13633 v Velocity[Y] -2.4904e-18 1.7115e-17 3.9825e-19 3.9825e-19 v Velocity[Z] -4.2049e-18 5.5208e-18 -8.183e-22 -8.183e-22 v ǁVelocityǁ 0.013671 0.87511 0.13633 0.13633 v Pressure 0 0 0 0 v CourantNb 0 3.089e-16 1.865e-17 1.865e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.175000000E+02 TIME STEP NUMBER 175 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16140E-11 0.11175E+00 Friction velocity uk : 0.16140E-11 0.11175E+00 Dimensionless distance yplus : 0.80701E-09 0.11175E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40393E-02 1515 0.90314E-08 0.11270E-04 0.16982E+00 c Velocity[X] 0.11270E-04 c Velocity[Y] 0.19394E-38 c Velocity[Z] 0.15762E-38 c Pressure 0.42235E-18 0 0.10000E+01 -0.42235E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01363 0.87548 0.13644 0.13644 v Velocity[Y] -2.5061e-18 1.7092e-17 3.9773e-19 3.9773e-19 v Velocity[Z] -4.2246e-18 5.5195e-18 -1.0596e-21 -1.0596e-21 v ǁVelocityǁ 0.01363 0.87548 0.13644 0.13644 v Pressure 0 0 0 0 v CourantNb 0 3.0986e-16 1.8675e-17 1.8675e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.176000000E+02 TIME STEP NUMBER 176 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18038E-11 0.11159E+00 Friction velocity uk : 0.18038E-11 0.11159E+00 Dimensionless distance yplus : 0.90191E-09 0.11159E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40436E-02 1515 0.89843E-08 0.11171E-04 0.16889E+00 c Velocity[X] 0.11171E-04 c Velocity[Y] 0.21014E-38 c Velocity[Z] 0.17085E-38 c Pressure 0.42304E-18 0 0.10000E+01 -0.42304E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013589 0.87584 0.13654 0.13654 v Velocity[Y] -2.5209e-18 1.7069e-17 3.9719e-19 3.9719e-19 v Velocity[Z] -4.2108e-18 5.5523e-18 -9.5834e-22 -9.5834e-22 v ǁVelocityǁ 0.013589 0.87584 0.13654 0.13654 v Pressure 0 0 0 0 v CourantNb 0 3.1035e-16 1.869e-17 1.869e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.177000000E+02 TIME STEP NUMBER 177 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19661E-11 0.11143E+00 Friction velocity uk : 0.19661E-11 0.11143E+00 Dimensionless distance yplus : 0.98304E-09 0.11143E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40480E-02 1514 0.90097E-08 0.11073E-04 0.16796E+00 c Velocity[X] 0.11073E-04 c Velocity[Y] 0.23508E-38 c Velocity[Z] 0.11846E-38 c Pressure 0.42354E-18 0 0.10000E+01 -0.42354E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013548 0.8762 0.13665 0.13665 v Velocity[Y] -2.5379e-18 1.7044e-17 3.9665e-19 3.9665e-19 v Velocity[Z] -4.2247e-18 5.5529e-18 -1.0445e-21 -1.0445e-21 v ǁVelocityǁ 0.013548 0.8762 0.13665 0.13665 v Pressure 0 0 0 0 v CourantNb 0 3.1023e-16 1.8724e-17 1.8724e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.178000000E+02 TIME STEP NUMBER 178 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18043E-11 0.11127E+00 Friction velocity uk : 0.18043E-11 0.11127E+00 Dimensionless distance yplus : 0.90214E-09 0.11127E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40523E-02 1513 0.90353E-08 0.10977E-04 0.16705E+00 c Velocity[X] 0.10977E-04 c Velocity[Y] 0.19575E-38 c Velocity[Z] 0.11363E-38 c Pressure 0.42413E-18 0 0.10000E+01 -0.42413E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013508 0.87655 0.13675 0.13675 v Velocity[Y] -2.5536e-18 1.7022e-17 3.9609e-19 3.9609e-19 v Velocity[Z] -4.231e-18 5.5575e-18 -8.8704e-22 -8.8704e-22 v ǁVelocityǁ 0.013508 0.87655 0.13675 0.13675 v Pressure 0 0 0 0 v CourantNb 0 3.1099e-16 1.8741e-17 1.8741e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.179000000E+02 TIME STEP NUMBER 179 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22295E-11 0.11111E+00 Friction velocity uk : 0.22295E-11 0.11111E+00 Dimensionless distance yplus : 0.11147E-08 0.11111E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40566E-02 1513 0.89890E-08 0.10882E-04 0.16614E+00 c Velocity[X] 0.10882E-04 c Velocity[Y] 0.18799E-38 c Velocity[Z] 0.16615E-38 c Pressure 0.42485E-18 0 0.10000E+01 -0.42485E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013469 0.87691 0.13685 0.13685 v Velocity[Y] -2.5689e-18 1.6999e-17 3.9552e-19 3.9552e-19 v Velocity[Z] -4.223e-18 5.5363e-18 -1.1814e-21 -1.1814e-21 v ǁVelocityǁ 0.013469 0.87691 0.13685 0.13685 v Pressure 0 0 0 0 v CourantNb 0 3.1105e-16 1.8772e-17 1.8772e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.180000000E+02 TIME STEP NUMBER 180 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21120E-11 0.11095E+00 Friction velocity uk : 0.21120E-11 0.11095E+00 Dimensionless distance yplus : 0.10560E-08 0.11095E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40609E-02 1512 0.90151E-08 0.10789E-04 0.16525E+00 c Velocity[X] 0.10789E-04 c Velocity[Y] 0.22521E-38 c Velocity[Z] 0.13867E-38 c Pressure 0.42538E-18 0 0.10000E+01 -0.42538E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013429 0.87725 0.13696 0.13696 v Velocity[Y] -2.5866e-18 1.6975e-17 3.9494e-19 3.9494e-19 v Velocity[Z] -4.2299e-18 5.534e-18 -1.4007e-21 -1.4007e-21 v ǁVelocityǁ 0.013429 0.87725 0.13696 0.13696 v Pressure 0 0 0 0 v CourantNb 0 3.1087e-16 1.8782e-17 1.8782e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.181000000E+02 TIME STEP NUMBER 181 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19917E-11 0.11079E+00 Friction velocity uk : 0.19917E-11 0.11079E+00 Dimensionless distance yplus : 0.99587E-09 0.11079E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40652E-02 1512 0.89693E-08 0.10697E-04 0.16436E+00 c Velocity[X] 0.10697E-04 c Velocity[Y] 0.22227E-38 c Velocity[Z] 0.14183E-38 c Pressure 0.42608E-18 0 0.10000E+01 -0.42608E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01339 0.8776 0.13706 0.13706 v Velocity[Y] -2.603e-18 1.6951e-17 3.9435e-19 3.9435e-19 v Velocity[Z] -4.2344e-18 5.556e-18 -1.2773e-21 -1.2773e-21 v ǁVelocityǁ 0.01339 0.8776 0.13706 0.13706 v Pressure 0 0 0 0 v CourantNb 0 3.1197e-16 1.8804e-17 1.8804e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.182000000E+02 TIME STEP NUMBER 182 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22532E-11 0.11063E+00 Friction velocity uk : 0.22532E-11 0.11063E+00 Dimensionless distance yplus : 0.11266E-08 0.11063E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40694E-02 1511 0.89958E-08 0.10606E-04 0.16349E+00 c Velocity[X] 0.10606E-04 c Velocity[Y] 0.22088E-38 c Velocity[Z] 0.12231E-38 c Pressure 0.42667E-18 0 0.10000E+01 -0.42667E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013352 0.87794 0.13716 0.13716 v Velocity[Y] -2.6199e-18 1.6927e-17 3.9375e-19 3.9375e-19 v Velocity[Z] -4.2432e-18 5.5593e-18 -1.1055e-21 -1.1055e-21 v ǁVelocityǁ 0.013352 0.87794 0.13716 0.13716 v Pressure 0 0 0 0 v CourantNb 0 3.1205e-16 1.8815e-17 1.8815e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.183000000E+02 TIME STEP NUMBER 183 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16250E-11 0.11048E+00 Friction velocity uk : 0.16250E-11 0.11048E+00 Dimensionless distance yplus : 0.81248E-09 0.11048E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40737E-02 1510 0.90227E-08 0.10516E-04 0.16262E+00 c Velocity[X] 0.10516E-04 c Velocity[Y] 0.19591E-38 c Velocity[Z] 0.22265E-38 c Pressure 0.42721E-18 0 0.10000E+01 -0.42721E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013313 0.87828 0.13727 0.13727 v Velocity[Y] -2.6353e-18 1.6906e-17 3.9313e-19 3.9313e-19 v Velocity[Z] -4.2449e-18 5.5797e-18 -7.524e-22 -7.524e-22 v ǁVelocityǁ 0.013313 0.87828 0.13727 0.13727 v Pressure 0 0 0 0 v CourantNb 0 3.1249e-16 1.8829e-17 1.8829e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.184000000E+02 TIME STEP NUMBER 184 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15402E-11 0.11033E+00 Friction velocity uk : 0.15402E-11 0.11033E+00 Dimensionless distance yplus : 0.77012E-09 0.11033E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40779E-02 1510 0.89776E-08 0.10428E-04 0.16176E+00 c Velocity[X] 0.10428E-04 c Velocity[Y] 0.18642E-38 c Velocity[Z] 0.19412E-38 c Pressure 0.42773E-18 0 0.10000E+01 -0.42773E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013275 0.87862 0.13737 0.13737 v Velocity[Y] -2.6533e-18 1.6883e-17 3.9251e-19 3.9251e-19 v Velocity[Z] -4.2521e-18 5.5453e-18 -8.3161e-22 -8.3161e-22 v ǁVelocityǁ 0.013275 0.87862 0.13737 0.13737 v Pressure 0 0 0 0 v CourantNb 0 3.1192e-16 1.886e-17 1.886e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.185000000E+02 TIME STEP NUMBER 185 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17804E-11 0.11017E+00 Friction velocity uk : 0.17804E-11 0.11017E+00 Dimensionless distance yplus : 0.89022E-09 0.11017E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40821E-02 1509 0.90048E-08 0.10341E-04 0.16091E+00 c Velocity[X] 0.10341E-04 c Velocity[Y] 0.19134E-38 c Velocity[Z] 0.16500E-38 c Pressure 0.42829E-18 0 0.10000E+01 -0.42829E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013237 0.87895 0.13747 0.13747 v Velocity[Y] -2.6707e-18 1.6859e-17 3.9189e-19 3.9189e-19 v Velocity[Z] -4.2186e-18 5.5526e-18 -5.1077e-22 -5.1077e-22 v ǁVelocityǁ 0.013237 0.87895 0.13747 0.13747 v Pressure 0 0 0 0 v CourantNb 0 3.1344e-16 1.8873e-17 1.8873e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.186000000E+02 TIME STEP NUMBER 186 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13855E-11 0.11002E+00 Friction velocity uk : 0.13855E-11 0.11002E+00 Dimensionless distance yplus : 0.69277E-09 0.11002E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40863E-02 1508 0.90324E-08 0.10255E-04 0.16007E+00 c Velocity[X] 0.10255E-04 c Velocity[Y] 0.24479E-38 c Velocity[Z] 0.15214E-38 c Pressure 0.42894E-18 0 0.10000E+01 -0.42894E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0132 0.87929 0.13757 0.13757 v Velocity[Y] -2.6861e-18 1.6834e-17 3.9125e-19 3.9125e-19 v Velocity[Z] -4.2443e-18 5.5538e-18 -5.9219e-22 -5.9219e-22 v ǁVelocityǁ 0.0132 0.87929 0.13757 0.13757 v Pressure 0 0 0 0 v CourantNb 0 3.1179e-16 1.8869e-17 1.8869e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.187000000E+02 TIME STEP NUMBER 187 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16910E-11 0.10987E+00 Friction velocity uk : 0.16910E-11 0.10987E+00 Dimensionless distance yplus : 0.84549E-09 0.10987E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40905E-02 1508 0.89879E-08 0.10170E-04 0.15924E+00 c Velocity[X] 0.10170E-04 c Velocity[Y] 0.20753E-38 c Velocity[Z] 0.16487E-38 c Pressure 0.42963E-18 0 0.10000E+01 -0.42963E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013163 0.87961 0.13768 0.13768 v Velocity[Y] -2.7042e-18 1.681e-17 3.906e-19 3.906e-19 v Velocity[Z] -4.2286e-18 5.5712e-18 -4.2699e-22 -4.2699e-22 v ǁVelocityǁ 0.013163 0.87961 0.13768 0.13768 v Pressure 0 0 0 0 v CourantNb 0 3.1282e-16 1.8893e-17 1.8893e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.188000000E+02 TIME STEP NUMBER 188 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12429E-11 0.10972E+00 Friction velocity uk : 0.12429E-11 0.10972E+00 Dimensionless distance yplus : 0.62146E-09 0.10972E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40946E-02 1507 0.90159E-08 0.10086E-04 0.15842E+00 c Velocity[X] 0.10086E-04 c Velocity[Y] 0.21905E-38 c Velocity[Z] 0.14391E-38 c Pressure 0.43012E-18 0 0.10000E+01 -0.43012E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013126 0.87994 0.13778 0.13778 v Velocity[Y] -2.7215e-18 1.6785e-17 3.8994e-19 3.8994e-19 v Velocity[Z] -4.2515e-18 5.5668e-18 -4.0577e-22 -4.0577e-22 v ǁVelocityǁ 0.013126 0.87994 0.13778 0.13778 v Pressure 0 0 0 0 v CourantNb 0 3.1295e-16 1.8919e-17 1.8919e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.189000000E+02 TIME STEP NUMBER 189 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14043E-11 0.10957E+00 Friction velocity uk : 0.14043E-11 0.10957E+00 Dimensionless distance yplus : 0.70216E-09 0.10957E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.40987E-02 1507 0.89719E-08 0.10004E-04 0.15761E+00 c Velocity[X] 0.10004E-04 c Velocity[Y] 0.21096E-38 c Velocity[Z] 0.18194E-38 c Pressure 0.43084E-18 0 0.10000E+01 -0.43084E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01309 0.88026 0.13788 0.13788 v Velocity[Y] -2.7382e-18 1.6761e-17 3.8928e-19 3.8928e-19 v Velocity[Z] -4.2498e-18 5.5742e-18 -5.6723e-22 -5.6723e-22 v ǁVelocityǁ 0.01309 0.88026 0.13788 0.13788 v Pressure 0 0 0 0 v CourantNb 0 3.1336e-16 1.894e-17 1.894e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.190000000E+02 TIME STEP NUMBER 190 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20018E-11 0.10942E+00 Friction velocity uk : 0.20018E-11 0.10942E+00 Dimensionless distance yplus : 0.10009E-08 0.10942E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41029E-02 1506 0.90002E-08 0.99226E-05 0.15680E+00 c Velocity[X] 0.99226E-05 c Velocity[Y] 0.22085E-38 c Velocity[Z] 0.17230E-38 c Pressure 0.43147E-18 0 0.10000E+01 -0.43147E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013053 0.88058 0.13798 0.13798 v Velocity[Y] -2.7555e-18 1.6736e-17 3.886e-19 3.886e-19 v Velocity[Z] -4.2653e-18 5.5814e-18 -5.0274e-22 -5.0274e-22 v ǁVelocityǁ 0.013053 0.88058 0.13798 0.13798 v Pressure 0 0 0 0 v CourantNb 0 3.1355e-16 1.8963e-17 1.8963e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.191000000E+02 TIME STEP NUMBER 191 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19053E-11 0.10928E+00 Friction velocity uk : 0.19053E-11 0.10928E+00 Dimensionless distance yplus : 0.95265E-09 0.10928E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41070E-02 1505 0.90289E-08 0.98423E-05 0.15601E+00 c Velocity[X] 0.98423E-05 c Velocity[Y] 0.23978E-38 c Velocity[Z] 0.11644E-38 c Pressure 0.43202E-18 0 0.10000E+01 -0.43202E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.013018 0.8809 0.13808 0.13808 v Velocity[Y] -2.7741e-18 1.6711e-17 3.8792e-19 3.8792e-19 v Velocity[Z] -4.247e-18 5.5833e-18 -7.6359e-22 -7.6359e-22 v ǁVelocityǁ 0.013018 0.8809 0.13808 0.13808 v Pressure 0 0 0 0 v CourantNb 0 3.1467e-16 1.8986e-17 1.8986e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.192000000E+02 TIME STEP NUMBER 192 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12059E-11 0.10913E+00 Friction velocity uk : 0.12059E-11 0.10913E+00 Dimensionless distance yplus : 0.60295E-09 0.10913E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41110E-02 1505 0.89855E-08 0.97631E-05 0.15522E+00 c Velocity[X] 0.97631E-05 c Velocity[Y] 0.21623E-38 c Velocity[Z] 0.14017E-38 c Pressure 0.43259E-18 0 0.10000E+01 -0.43259E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012982 0.88122 0.13818 0.13818 v Velocity[Y] -2.7909e-18 1.6685e-17 3.8722e-19 3.8722e-19 v Velocity[Z] -4.2581e-18 5.5859e-18 -6.483e-22 -6.483e-22 v ǁVelocityǁ 0.012982 0.88122 0.13818 0.13818 v Pressure 0 0 0 0 v CourantNb 0 3.1415e-16 1.9004e-17 1.9004e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.193000000E+02 TIME STEP NUMBER 193 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86878E-12 0.10899E+00 Friction velocity uk : 0.86878E-12 0.10899E+00 Dimensionless distance yplus : 0.43439E-09 0.10899E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41151E-02 1504 0.90145E-08 0.96849E-05 0.15444E+00 c Velocity[X] 0.96849E-05 c Velocity[Y] 0.24284E-38 c Velocity[Z] 0.16838E-38 c Pressure 0.43301E-18 0 0.10000E+01 -0.43301E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012947 0.88153 0.13828 0.13828 v Velocity[Y] -2.8091e-18 1.6658e-17 3.8652e-19 3.8652e-19 v Velocity[Z] -4.2357e-18 5.5815e-18 -7.2168e-22 -7.2168e-22 v ǁVelocityǁ 0.012947 0.88153 0.13828 0.13828 v Pressure 0 0 0 0 v CourantNb 0 3.1449e-16 1.9014e-17 1.9014e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.194000000E+02 TIME STEP NUMBER 194 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10882E-11 0.10884E+00 Friction velocity uk : 0.10882E-11 0.10884E+00 Dimensionless distance yplus : 0.54412E-09 0.10884E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41192E-02 1504 0.89717E-08 0.96078E-05 0.15367E+00 c Velocity[X] 0.96078E-05 c Velocity[Y] 0.22110E-38 c Velocity[Z] 0.15625E-38 c Pressure 0.43380E-18 0 0.10000E+01 -0.43380E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012912 0.88184 0.13838 0.13838 v Velocity[Y] -2.8264e-18 1.6636e-17 3.858e-19 3.858e-19 v Velocity[Z] -4.2528e-18 5.598e-18 -1.1023e-21 -1.1023e-21 v ǁVelocityǁ 0.012912 0.88184 0.13838 0.13838 v Pressure 0 0 0 0 v CourantNb 0 3.1467e-16 1.9023e-17 1.9023e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.195000000E+02 TIME STEP NUMBER 195 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17234E-11 0.10870E+00 Friction velocity uk : 0.17234E-11 0.10870E+00 Dimensionless distance yplus : 0.86169E-09 0.10870E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41232E-02 1503 0.90011E-08 0.95316E-05 0.15290E+00 c Velocity[X] 0.95316E-05 c Velocity[Y] 0.23733E-38 c Velocity[Z] 0.18720E-38 c Pressure 0.43439E-18 0 0.10000E+01 -0.43439E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012877 0.88215 0.13848 0.13848 v Velocity[Y] -2.8439e-18 1.6609e-17 3.8508e-19 3.8508e-19 v Velocity[Z] -4.2731e-18 5.6132e-18 -6.9875e-22 -6.9875e-22 v ǁVelocityǁ 0.012877 0.88215 0.13848 0.13848 v Pressure 0 0 0 0 v CourantNb 0 3.1521e-16 1.9052e-17 1.9052e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.196000000E+02 TIME STEP NUMBER 196 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21922E-11 0.10856E+00 Friction velocity uk : 0.21922E-11 0.10856E+00 Dimensionless distance yplus : 0.10961E-08 0.10856E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41272E-02 1502 0.90307E-08 0.94565E-05 0.15214E+00 c Velocity[X] 0.94565E-05 c Velocity[Y] 0.19460E-38 c Velocity[Z] 0.20265E-38 c Pressure 0.43488E-18 0 0.10000E+01 -0.43488E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012842 0.88245 0.13858 0.13858 v Velocity[Y] -2.8607e-18 1.6586e-17 3.8435e-19 3.8435e-19 v Velocity[Z] -4.2632e-18 5.5982e-18 -1.035e-21 -1.035e-21 v ǁVelocityǁ 0.012842 0.88245 0.13858 0.13858 v Pressure 0 0 0 0 v CourantNb 0 3.1533e-16 1.9086e-17 1.9086e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.197000000E+02 TIME STEP NUMBER 197 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17765E-11 0.10842E+00 Friction velocity uk : 0.17765E-11 0.10842E+00 Dimensionless distance yplus : 0.88826E-09 0.10842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41312E-02 1502 0.89884E-08 0.93823E-05 0.15139E+00 c Velocity[X] 0.93823E-05 c Velocity[Y] 0.22792E-38 c Velocity[Z] 0.17840E-38 c Pressure 0.43566E-18 0 0.10000E+01 -0.43566E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012808 0.88276 0.13868 0.13868 v Velocity[Y] -2.8776e-18 1.6561e-17 3.836e-19 3.836e-19 v Velocity[Z] -4.2773e-18 5.5847e-18 -9.2138e-22 -9.2138e-22 v ǁVelocityǁ 0.012808 0.88276 0.13868 0.13868 v Pressure 0 0 0 0 v CourantNb 0 3.1512e-16 1.9112e-17 1.9112e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.198000000E+02 TIME STEP NUMBER 198 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11392E-11 0.10828E+00 Friction velocity uk : 0.11392E-11 0.10828E+00 Dimensionless distance yplus : 0.56960E-09 0.10828E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41352E-02 1501 0.90185E-08 0.93091E-05 0.15065E+00 c Velocity[X] 0.93091E-05 c Velocity[Y] 0.20526E-38 c Velocity[Z] 0.21862E-38 c Pressure 0.43618E-18 0 0.10000E+01 -0.43618E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012774 0.88306 0.13878 0.13878 v Velocity[Y] -2.8947e-18 1.6537e-17 3.8285e-19 3.8285e-19 v Velocity[Z] -4.2863e-18 5.6207e-18 -1.2724e-21 -1.2724e-21 v ǁVelocityǁ 0.012774 0.88306 0.13878 0.13878 v Pressure 0 0 0 0 v CourantNb 0 3.1622e-16 1.9121e-17 1.9121e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.199000000E+02 TIME STEP NUMBER 199 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23310E-11 0.10814E+00 Friction velocity uk : 0.23310E-11 0.10814E+00 Dimensionless distance yplus : 0.11655E-08 0.10814E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41392E-02 1501 0.89766E-08 0.92368E-05 0.14992E+00 c Velocity[X] 0.92368E-05 c Velocity[Y] 0.17920E-38 c Velocity[Z] 0.15325E-38 c Pressure 0.43684E-18 0 0.10000E+01 -0.43684E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01274 0.88336 0.13887 0.13887 v Velocity[Y] -2.9127e-18 1.6515e-17 3.8209e-19 3.8209e-19 v Velocity[Z] -4.3139e-18 5.6191e-18 -1.3423e-21 -1.3423e-21 v ǁVelocityǁ 0.01274 0.88336 0.13887 0.13887 v Pressure 0 0 0 0 v CourantNb 0 3.1729e-16 1.9161e-17 1.9161e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.200000000E+02 TIME STEP NUMBER 200 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23972E-11 0.10800E+00 Friction velocity uk : 0.23972E-11 0.10800E+00 Dimensionless distance yplus : 0.11986E-08 0.10800E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 200, Physical time 0.20000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41432E-02 1500 0.90070E-08 0.91654E-05 0.14919E+00 c Velocity[X] 0.91654E-05 c Velocity[Y] 0.20786E-38 c Velocity[Z] 0.20228E-38 c Pressure 0.43750E-18 0 0.10000E+01 -0.43750E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012707 0.88365 0.13897 0.13897 v Velocity[Y] -2.9291e-18 1.6491e-17 3.8132e-19 3.8132e-19 v Velocity[Z] -4.2912e-18 5.6168e-18 -1.1603e-21 -1.1603e-21 v ǁVelocityǁ 0.012707 0.88365 0.13897 0.13897 v Pressure 0 0 0 0 v CourantNb 0 3.1724e-16 1.9181e-17 1.9181e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.201000000E+02 TIME STEP NUMBER 201 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18550E-11 0.10787E+00 Friction velocity uk : 0.18550E-11 0.10787E+00 Dimensionless distance yplus : 0.92752E-09 0.10787E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41471E-02 1499 0.90377E-08 0.90949E-05 0.14847E+00 c Velocity[X] 0.90949E-05 c Velocity[Y] 0.21742E-38 c Velocity[Z] 0.14985E-38 c Pressure 0.43793E-18 0 0.10000E+01 -0.43793E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012674 0.88394 0.13907 0.13907 v Velocity[Y] -2.9477e-18 1.6466e-17 3.8055e-19 3.8055e-19 v Velocity[Z] -4.29e-18 5.6212e-18 -1.3326e-21 -1.3326e-21 v ǁVelocityǁ 0.012674 0.88394 0.13907 0.13907 v Pressure 0 0 0 0 v CourantNb 0 3.1731e-16 1.9209e-17 1.9209e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.202000000E+02 TIME STEP NUMBER 202 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19278E-11 0.10773E+00 Friction velocity uk : 0.19278E-11 0.10773E+00 Dimensionless distance yplus : 0.96391E-09 0.10773E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41511E-02 1499 0.89963E-08 0.90254E-05 0.14775E+00 c Velocity[X] 0.90254E-05 c Velocity[Y] 0.17669E-38 c Velocity[Z] 0.28342E-38 c Pressure 0.43865E-18 0 0.10000E+01 -0.43865E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012641 0.88424 0.13917 0.13917 v Velocity[Y] -2.966e-18 1.6446e-17 3.7977e-19 3.7977e-19 v Velocity[Z] -4.2906e-18 5.6158e-18 -8.4962e-22 -8.4962e-22 v ǁVelocityǁ 0.012641 0.88424 0.13917 0.13917 v Pressure 0 0 0 0 v CourantNb 0 3.1761e-16 1.9221e-17 1.9221e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.203000000E+02 TIME STEP NUMBER 203 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19219E-11 0.10759E+00 Friction velocity uk : 0.19219E-11 0.10759E+00 Dimensionless distance yplus : 0.96093E-09 0.10759E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41550E-02 1498 0.90274E-08 0.89567E-05 0.14705E+00 c Velocity[X] 0.89567E-05 c Velocity[Y] 0.15906E-38 c Velocity[Z] 0.22564E-38 c Pressure 0.43918E-18 0 0.10000E+01 -0.43918E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012608 0.88452 0.13927 0.13927 v Velocity[Y] -2.9856e-18 1.6429e-17 3.7898e-19 3.7898e-19 v Velocity[Z] -4.3021e-18 5.6621e-18 -7.3988e-22 -7.3988e-22 v ǁVelocityǁ 0.012608 0.88452 0.13927 0.13927 v Pressure 0 0 0 0 v CourantNb 0 3.173e-16 1.9243e-17 1.9243e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.204000000E+02 TIME STEP NUMBER 204 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13539E-11 0.10746E+00 Friction velocity uk : 0.13539E-11 0.10746E+00 Dimensionless distance yplus : 0.67697E-09 0.10746E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41589E-02 1498 0.89865E-08 0.88888E-05 0.14635E+00 c Velocity[X] 0.88888E-05 c Velocity[Y] 0.18415E-38 c Velocity[Z] 0.16921E-38 c Pressure 0.43974E-18 0 0.10000E+01 -0.43974E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012576 0.88481 0.13936 0.13936 v Velocity[Y] -3.0041e-18 1.6409e-17 3.7818e-19 3.7818e-19 v Velocity[Z] -4.2956e-18 5.6361e-18 -8.2139e-22 -8.2139e-22 v ǁVelocityǁ 0.012576 0.88481 0.13936 0.13936 v Pressure 0 0 0 0 v CourantNb 0 3.1801e-16 1.9277e-17 1.9277e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.205000000E+02 TIME STEP NUMBER 205 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14958E-11 0.10733E+00 Friction velocity uk : 0.14958E-11 0.10733E+00 Dimensionless distance yplus : 0.74791E-09 0.10733E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41628E-02 1497 0.90179E-08 0.88218E-05 0.14565E+00 c Velocity[X] 0.88218E-05 c Velocity[Y] 0.19084E-38 c Velocity[Z] 0.17510E-38 c Pressure 0.44042E-18 0 0.10000E+01 -0.44042E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012544 0.8851 0.13946 0.13946 v Velocity[Y] -3.0214e-18 1.6388e-17 3.7738e-19 3.7738e-19 v Velocity[Z] -4.296e-18 5.6607e-18 -6.8833e-22 -6.8833e-22 v ǁVelocityǁ 0.012544 0.8851 0.13946 0.13946 v Pressure 0 0 0 0 v CourantNb 0 3.1772e-16 1.9308e-17 1.9308e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.206000000E+02 TIME STEP NUMBER 206 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16685E-11 0.10719E+00 Friction velocity uk : 0.16685E-11 0.10719E+00 Dimensionless distance yplus : 0.83423E-09 0.10719E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41667E-02 1497 0.89773E-08 0.87557E-05 0.14497E+00 c Velocity[X] 0.87557E-05 c Velocity[Y] 0.18396E-38 c Velocity[Z] 0.14945E-38 c Pressure 0.44100E-18 0 0.10000E+01 -0.44100E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012512 0.88538 0.13956 0.13956 v Velocity[Y] -3.0399e-18 1.6367e-17 3.7657e-19 3.7657e-19 v Velocity[Z] -4.3193e-18 5.6619e-18 -9.9961e-22 -9.9961e-22 v ǁVelocityǁ 0.012512 0.88538 0.13956 0.13956 v Pressure 0 0 0 0 v CourantNb 0 3.1936e-16 1.9322e-17 1.9322e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.207000000E+02 TIME STEP NUMBER 207 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21280E-11 0.10706E+00 Friction velocity uk : 0.21280E-11 0.10706E+00 Dimensionless distance yplus : 0.10640E-08 0.10706E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41705E-02 1496 0.90091E-08 0.86903E-05 0.14429E+00 c Velocity[X] 0.86903E-05 c Velocity[Y] 0.19427E-38 c Velocity[Z] 0.21747E-38 c Pressure 0.44150E-18 0 0.10000E+01 -0.44150E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01248 0.88566 0.13965 0.13965 v Velocity[Y] -3.0583e-18 1.6347e-17 3.7575e-19 3.7575e-19 v Velocity[Z] -4.3105e-18 5.6693e-18 -1.4547e-21 -1.4547e-21 v ǁVelocityǁ 0.01248 0.88566 0.13965 0.13965 v Pressure 0 0 0 0 v CourantNb 0 3.1924e-16 1.934e-17 1.934e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.208000000E+02 TIME STEP NUMBER 208 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21032E-11 0.10693E+00 Friction velocity uk : 0.21032E-11 0.10693E+00 Dimensionless distance yplus : 0.10516E-08 0.10693E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41744E-02 1495 0.90411E-08 0.86257E-05 0.14361E+00 c Velocity[X] 0.86257E-05 c Velocity[Y] 0.15416E-38 c Velocity[Z] 0.26561E-38 c Pressure 0.44206E-18 0 0.10000E+01 -0.44206E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012449 0.88594 0.13975 0.13975 v Velocity[Y] -3.0765e-18 1.6329e-17 3.7493e-19 3.7493e-19 v Velocity[Z] -4.2979e-18 5.6775e-18 -8.5003e-22 -8.5003e-22 v ǁVelocityǁ 0.012449 0.88594 0.13975 0.13975 v Pressure 0 0 0 0 v CourantNb 0 3.1995e-16 1.9365e-17 1.9365e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.209000000E+02 TIME STEP NUMBER 209 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24693E-11 0.10680E+00 Friction velocity uk : 0.24693E-11 0.10680E+00 Dimensionless distance yplus : 0.12346E-08 0.10680E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41782E-02 1495 0.90010E-08 0.85620E-05 0.14295E+00 c Velocity[X] 0.85620E-05 c Velocity[Y] 0.16918E-38 c Velocity[Z] 0.16242E-38 c Pressure 0.44250E-18 0 0.10000E+01 -0.44250E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012417 0.88621 0.13984 0.13984 v Velocity[Y] -3.0948e-18 1.6307e-17 3.7411e-19 3.7411e-19 v Velocity[Z] -4.2905e-18 5.6705e-18 -5.5642e-22 -5.5642e-22 v ǁVelocityǁ 0.012417 0.88621 0.13984 0.13984 v Pressure 0 0 0 0 v CourantNb 0 3.1813e-16 1.9388e-17 1.9388e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.210000000E+02 TIME STEP NUMBER 210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22853E-11 0.10667E+00 Friction velocity uk : 0.22853E-11 0.10667E+00 Dimensionless distance yplus : 0.11427E-08 0.10667E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41820E-02 1494 0.90334E-08 0.84990E-05 0.14229E+00 c Velocity[X] 0.84990E-05 c Velocity[Y] 0.17838E-38 c Velocity[Z] 0.21504E-38 c Pressure 0.44316E-18 0 0.10000E+01 -0.44316E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012386 0.88649 0.13994 0.13994 v Velocity[Y] -3.1137e-18 1.6288e-17 3.7328e-19 3.7328e-19 v Velocity[Z] -4.3064e-18 5.6735e-18 -7.7035e-22 -7.7035e-22 v ǁVelocityǁ 0.012386 0.88649 0.13994 0.13994 v Pressure 0 0 0 0 v CourantNb 0 3.1837e-16 1.939e-17 1.939e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.211000000E+02 TIME STEP NUMBER 211 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24870E-11 0.10654E+00 Friction velocity uk : 0.24870E-11 0.10654E+00 Dimensionless distance yplus : 0.12435E-08 0.10654E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41858E-02 1494 0.89937E-08 0.84367E-05 0.14163E+00 c Velocity[X] 0.84367E-05 c Velocity[Y] 0.18389E-38 c Velocity[Z] 0.20084E-38 c Pressure 0.44370E-18 0 0.10000E+01 -0.44370E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012356 0.88676 0.14003 0.14003 v Velocity[Y] -3.1329e-18 1.6266e-17 3.7245e-19 3.7245e-19 v Velocity[Z] -4.3049e-18 5.6677e-18 -6.2866e-22 -6.2866e-22 v ǁVelocityǁ 0.012356 0.88676 0.14003 0.14003 v Pressure 0 0 0 0 v CourantNb 0 3.2003e-16 1.9424e-17 1.9424e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.212000000E+02 TIME STEP NUMBER 212 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22195E-11 0.10641E+00 Friction velocity uk : 0.22195E-11 0.10641E+00 Dimensionless distance yplus : 0.11098E-08 0.10641E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41896E-02 1493 0.90264E-08 0.83752E-05 0.14098E+00 c Velocity[X] 0.83752E-05 c Velocity[Y] 0.18587E-38 c Velocity[Z] 0.13439E-38 c Pressure 0.44421E-18 0 0.10000E+01 -0.44421E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012325 0.88703 0.14013 0.14013 v Velocity[Y] -3.151e-18 1.6245e-17 3.7161e-19 3.7161e-19 v Velocity[Z] -4.2958e-18 5.6614e-18 -9.9335e-22 -9.9335e-22 v ǁVelocityǁ 0.012325 0.88703 0.14013 0.14013 v Pressure 0 0 0 0 v CourantNb 0 3.195e-16 1.943e-17 1.943e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.213000000E+02 TIME STEP NUMBER 213 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22674E-11 0.10629E+00 Friction velocity uk : 0.22674E-11 0.10629E+00 Dimensionless distance yplus : 0.11337E-08 0.10629E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41934E-02 1493 0.89871E-08 0.83145E-05 0.14034E+00 c Velocity[X] 0.83145E-05 c Velocity[Y] 0.17019E-38 c Velocity[Z] 0.27776E-38 c Pressure 0.44501E-18 0 0.10000E+01 -0.44501E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012295 0.8873 0.14022 0.14022 v Velocity[Y] -3.1701e-18 1.6225e-17 3.7077e-19 3.7077e-19 v Velocity[Z] -4.318e-18 5.6821e-18 -2.4816e-22 -2.4816e-22 v ǁVelocityǁ 0.012295 0.8873 0.14022 0.14022 v Pressure 0 0 0 0 v CourantNb 0 3.1951e-16 1.9445e-17 1.9445e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.214000000E+02 TIME STEP NUMBER 214 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26523E-11 0.10616E+00 Friction velocity uk : 0.26523E-11 0.10616E+00 Dimensionless distance yplus : 0.13262E-08 0.10616E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.41972E-02 1492 0.90201E-08 0.82544E-05 0.13970E+00 c Velocity[X] 0.82544E-05 c Velocity[Y] 0.17621E-38 c Velocity[Z] 0.23757E-38 c Pressure 0.44536E-18 0 0.10000E+01 -0.44536E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012265 0.88756 0.14032 0.14032 v Velocity[Y] -3.1902e-18 1.6207e-17 3.6992e-19 3.6992e-19 v Velocity[Z] -4.3116e-18 5.6807e-18 -5.9889e-22 -5.9889e-22 v ǁVelocityǁ 0.012265 0.88756 0.14032 0.14032 v Pressure 0 0 0 0 v CourantNb 0 3.2056e-16 1.9471e-17 1.9471e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.215000000E+02 TIME STEP NUMBER 215 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28897E-11 0.10604E+00 Friction velocity uk : 0.28897E-11 0.10604E+00 Dimensionless distance yplus : 0.14448E-08 0.10604E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42009E-02 1492 0.89812E-08 0.81951E-05 0.13907E+00 c Velocity[X] 0.81951E-05 c Velocity[Y] 0.20105E-38 c Velocity[Z] 0.16176E-38 c Pressure 0.44596E-18 0 0.10000E+01 -0.44596E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012235 0.88783 0.14041 0.14041 v Velocity[Y] -3.21e-18 1.6184e-17 3.6906e-19 3.6906e-19 v Velocity[Z] -4.3011e-18 5.6947e-18 -8.4108e-22 -8.4108e-22 v ǁVelocityǁ 0.012235 0.88783 0.14041 0.14041 v Pressure 0 0 0 0 v CourantNb 0 3.2052e-16 1.95e-17 1.95e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.216000000E+02 TIME STEP NUMBER 216 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25897E-11 0.10591E+00 Friction velocity uk : 0.25897E-11 0.10591E+00 Dimensionless distance yplus : 0.12949E-08 0.10591E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42047E-02 1491 0.90145E-08 0.81365E-05 0.13845E+00 c Velocity[X] 0.81365E-05 c Velocity[Y] 0.19842E-38 c Velocity[Z] 0.17174E-38 c Pressure 0.44648E-18 0 0.10000E+01 -0.44648E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012205 0.88809 0.14051 0.14051 v Velocity[Y] -3.2289e-18 1.6161e-17 3.682e-19 3.682e-19 v Velocity[Z] -4.3273e-18 5.682e-18 -7.6075e-22 -7.6075e-22 v ǁVelocityǁ 0.012205 0.88809 0.14051 0.14051 v Pressure 0 0 0 0 v CourantNb 0 3.2016e-16 1.95e-17 1.95e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.217000000E+02 TIME STEP NUMBER 217 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27720E-11 0.10579E+00 Friction velocity uk : 0.27720E-11 0.10579E+00 Dimensionless distance yplus : 0.13860E-08 0.10579E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42084E-02 1491 0.89760E-08 0.80786E-05 0.13783E+00 c Velocity[X] 0.80786E-05 c Velocity[Y] 0.18283E-38 c Velocity[Z] 0.21155E-38 c Pressure 0.44703E-18 0 0.10000E+01 -0.44703E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012176 0.88835 0.1406 0.1406 v Velocity[Y] -3.2465e-18 1.614e-17 3.6732e-19 3.6732e-19 v Velocity[Z] -4.3243e-18 5.6895e-18 -2.9702e-22 -2.9702e-22 v ǁVelocityǁ 0.012176 0.88835 0.1406 0.1406 v Pressure 0 0 0 0 v CourantNb 0 3.214e-16 1.9518e-17 1.9518e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.218000000E+02 TIME STEP NUMBER 218 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28678E-11 0.10566E+00 Friction velocity uk : 0.28678E-11 0.10566E+00 Dimensionless distance yplus : 0.14339E-08 0.10566E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42121E-02 1490 0.90096E-08 0.80213E-05 0.13721E+00 c Velocity[X] 0.80213E-05 c Velocity[Y] 0.16873E-38 c Velocity[Z] 0.26743E-38 c Pressure 0.44755E-18 0 0.10000E+01 -0.44755E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012146 0.88861 0.14069 0.14069 v Velocity[Y] -3.2648e-18 1.6121e-17 3.6645e-19 3.6645e-19 v Velocity[Z] -4.3084e-18 5.6856e-18 -3.3072e-22 -3.3072e-22 v ǁVelocityǁ 0.012146 0.88861 0.14069 0.14069 v Pressure 0 0 0 0 v CourantNb 0 3.2036e-16 1.9526e-17 1.9526e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.219000000E+02 TIME STEP NUMBER 219 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29451E-11 0.10554E+00 Friction velocity uk : 0.29451E-11 0.10554E+00 Dimensionless distance yplus : 0.14725E-08 0.10554E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42158E-02 1490 0.89714E-08 0.79647E-05 0.13660E+00 c Velocity[X] 0.79647E-05 c Velocity[Y] 0.16920E-38 c Velocity[Z] 0.23521E-38 c Pressure 0.44812E-18 0 0.10000E+01 -0.44812E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012117 0.88887 0.14079 0.14079 v Velocity[Y] -3.2841e-18 1.6102e-17 3.6556e-19 3.6556e-19 v Velocity[Z] -4.3074e-18 5.698e-18 -3.6111e-22 -3.6111e-22 v ǁVelocityǁ 0.012117 0.88887 0.14079 0.14079 v Pressure 0 0 0 0 v CourantNb 0 3.2019e-16 1.9556e-17 1.9556e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.220000000E+02 TIME STEP NUMBER 220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29866E-11 0.10542E+00 Friction velocity uk : 0.29866E-11 0.10542E+00 Dimensionless distance yplus : 0.14933E-08 0.10542E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42195E-02 1489 0.90054E-08 0.79088E-05 0.13600E+00 c Velocity[X] 0.79088E-05 c Velocity[Y] 0.19565E-38 c Velocity[Z] 0.18998E-38 c Pressure 0.44865E-18 0 0.10000E+01 -0.44865E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012088 0.88912 0.14088 0.14088 v Velocity[Y] -3.3019e-18 1.608e-17 3.6467e-19 3.6467e-19 v Velocity[Z] -4.3255e-18 5.7095e-18 -3.5274e-22 -3.5274e-22 v ǁVelocityǁ 0.012088 0.88912 0.14088 0.14088 v Pressure 0 0 0 0 v CourantNb 0 3.2074e-16 1.9577e-17 1.9577e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.221000000E+02 TIME STEP NUMBER 221 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27397E-11 0.10530E+00 Friction velocity uk : 0.27397E-11 0.10530E+00 Dimensionless distance yplus : 0.13699E-08 0.10530E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42232E-02 1488 0.90396E-08 0.78535E-05 0.13540E+00 c Velocity[X] 0.78535E-05 c Velocity[Y] 0.16734E-38 c Velocity[Z] 0.18510E-38 c Pressure 0.44918E-18 0 0.10000E+01 -0.44918E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01206 0.88937 0.14097 0.14097 v Velocity[Y] -3.3208e-18 1.606e-17 3.6378e-19 3.6378e-19 v Velocity[Z] -4.3106e-18 5.6936e-18 -7.4707e-22 -7.4707e-22 v ǁVelocityǁ 0.01206 0.88937 0.14097 0.14097 v Pressure 0 0 0 0 v CourantNb 0 3.2097e-16 1.9596e-17 1.9596e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.222000000E+02 TIME STEP NUMBER 222 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28958E-11 0.10518E+00 Friction velocity uk : 0.28958E-11 0.10518E+00 Dimensionless distance yplus : 0.14479E-08 0.10518E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42268E-02 1488 0.90018E-08 0.77988E-05 0.13481E+00 c Velocity[X] 0.77988E-05 c Velocity[Y] 0.19169E-38 c Velocity[Z] 0.22920E-38 c Pressure 0.44983E-18 0 0.10000E+01 -0.44983E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012031 0.88962 0.14107 0.14107 v Velocity[Y] -3.3393e-18 1.6041e-17 3.6287e-19 3.6287e-19 v Velocity[Z] -4.3299e-18 5.7168e-18 -4.758e-22 -4.758e-22 v ǁVelocityǁ 0.012031 0.88962 0.14107 0.14107 v Pressure 0 0 0 0 v CourantNb 0 3.2226e-16 1.9608e-17 1.9608e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.223000000E+02 TIME STEP NUMBER 223 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26690E-11 0.10506E+00 Friction velocity uk : 0.26690E-11 0.10506E+00 Dimensionless distance yplus : 0.13345E-08 0.10506E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42305E-02 1487 0.90363E-08 0.77448E-05 0.13422E+00 c Velocity[X] 0.77448E-05 c Velocity[Y] 0.19758E-38 c Velocity[Z] 0.17692E-38 c Pressure 0.45024E-18 0 0.10000E+01 -0.45024E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.012003 0.88987 0.14116 0.14116 v Velocity[Y] -3.3582e-18 1.6018e-17 3.6196e-19 3.6196e-19 v Velocity[Z] -4.298e-18 5.7059e-18 -8.7305e-22 -8.7305e-22 v ǁVelocityǁ 0.012003 0.88987 0.14116 0.14116 v Pressure 0 0 0 0 v CourantNb 0 3.2143e-16 1.9641e-17 1.9641e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.224000000E+02 TIME STEP NUMBER 224 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29741E-11 0.10494E+00 Friction velocity uk : 0.29741E-11 0.10494E+00 Dimensionless distance yplus : 0.14871E-08 0.10494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42341E-02 1487 0.89988E-08 0.76913E-05 0.13364E+00 c Velocity[X] 0.76913E-05 c Velocity[Y] 0.18951E-38 c Velocity[Z] 0.18553E-38 c Pressure 0.45088E-18 0 0.10000E+01 -0.45088E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011975 0.89012 0.14125 0.14125 v Velocity[Y] -3.3767e-18 1.5994e-17 3.6105e-19 3.6105e-19 v Velocity[Z] -4.3195e-18 5.7146e-18 -7.6631e-22 -7.6631e-22 v ǁVelocityǁ 0.011975 0.89012 0.14125 0.14125 v Pressure 0 0 0 0 v CourantNb 0 3.2114e-16 1.9656e-17 1.9656e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.225000000E+02 TIME STEP NUMBER 225 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25698E-11 0.10482E+00 Friction velocity uk : 0.25698E-11 0.10482E+00 Dimensionless distance yplus : 0.12849E-08 0.10482E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42378E-02 1486 0.90337E-08 0.76385E-05 0.13306E+00 c Velocity[X] 0.76385E-05 c Velocity[Y] 0.19321E-38 c Velocity[Z] 0.16903E-38 c Pressure 0.45131E-18 0 0.10000E+01 -0.45131E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011947 0.89037 0.14134 0.14134 v Velocity[Y] -3.3956e-18 1.5975e-17 3.6012e-19 3.6012e-19 v Velocity[Z] -4.31e-18 5.7126e-18 -7.4997e-22 -7.4997e-22 v ǁVelocityǁ 0.011947 0.89037 0.14134 0.14134 v Pressure 0 0 0 0 v CourantNb 0 3.2179e-16 1.966e-17 1.966e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.226000000E+02 TIME STEP NUMBER 226 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29647E-11 0.10471E+00 Friction velocity uk : 0.29647E-11 0.10471E+00 Dimensionless distance yplus : 0.14824E-08 0.10471E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42414E-02 1486 0.89965E-08 0.75863E-05 0.13249E+00 c Velocity[X] 0.75863E-05 c Velocity[Y] 0.18047E-38 c Velocity[Z] 0.17309E-38 c Pressure 0.45180E-18 0 0.10000E+01 -0.45180E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011919 0.89061 0.14144 0.14144 v Velocity[Y] -3.4154e-18 1.5955e-17 3.5919e-19 3.5919e-19 v Velocity[Z] -4.325e-18 5.7255e-18 -8.2986e-22 -8.2986e-22 v ǁVelocityǁ 0.011919 0.89061 0.14144 0.14144 v Pressure 0 0 0 0 v CourantNb 0 3.2238e-16 1.9686e-17 1.9686e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.227000000E+02 TIME STEP NUMBER 227 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27451E-11 0.10459E+00 Friction velocity uk : 0.27451E-11 0.10459E+00 Dimensionless distance yplus : 0.13726E-08 0.10459E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42450E-02 1485 0.90316E-08 0.75346E-05 0.13192E+00 c Velocity[X] 0.75346E-05 c Velocity[Y] 0.18654E-38 c Velocity[Z] 0.17151E-38 c Pressure 0.45241E-18 0 0.10000E+01 -0.45241E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011892 0.89085 0.14153 0.14153 v Velocity[Y] -3.4333e-18 1.5936e-17 3.5825e-19 3.5825e-19 v Velocity[Z] -4.3315e-18 5.7301e-18 -8.284e-22 -8.284e-22 v ǁVelocityǁ 0.011892 0.89085 0.14153 0.14153 v Pressure 0 0 0 0 v CourantNb 0 3.23e-16 1.9702e-17 1.9702e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.228000000E+02 TIME STEP NUMBER 228 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31085E-11 0.10447E+00 Friction velocity uk : 0.31085E-11 0.10447E+00 Dimensionless distance yplus : 0.15543E-08 0.10447E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42486E-02 1485 0.89948E-08 0.74836E-05 0.13136E+00 c Velocity[X] 0.74836E-05 c Velocity[Y] 0.17795E-38 c Velocity[Z] 0.24887E-38 c Pressure 0.45302E-18 0 0.10000E+01 -0.45302E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011865 0.8911 0.14162 0.14162 v Velocity[Y] -3.452e-18 1.5916e-17 3.573e-19 3.573e-19 v Velocity[Z] -4.3612e-18 5.7325e-18 -1.1023e-21 -1.1023e-21 v ǁVelocityǁ 0.011865 0.8911 0.14162 0.14162 v Pressure 0 0 0 0 v CourantNb 0 3.2293e-16 1.974e-17 1.974e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.229000000E+02 TIME STEP NUMBER 229 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31162E-11 0.10436E+00 Friction velocity uk : 0.31162E-11 0.10436E+00 Dimensionless distance yplus : 0.15581E-08 0.10436E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42522E-02 1484 0.90302E-08 0.74331E-05 0.13080E+00 c Velocity[X] 0.74331E-05 c Velocity[Y] 0.17703E-38 c Velocity[Z] 0.19545E-38 c Pressure 0.45340E-18 0 0.10000E+01 -0.45340E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011837 0.89134 0.14171 0.14171 v Velocity[Y] -3.4703e-18 1.5896e-17 3.5634e-19 3.5634e-19 v Velocity[Z] -4.3339e-18 5.7209e-18 -9.7116e-22 -9.7116e-22 v ǁVelocityǁ 0.011837 0.89134 0.14171 0.14171 v Pressure 0 0 0 0 v CourantNb 0 3.2393e-16 1.976e-17 1.976e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.230000000E+02 TIME STEP NUMBER 230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30558E-11 0.10424E+00 Friction velocity uk : 0.30558E-11 0.10424E+00 Dimensionless distance yplus : 0.15279E-08 0.10424E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42557E-02 1484 0.89937E-08 0.73831E-05 0.13025E+00 c Velocity[X] 0.73831E-05 c Velocity[Y] 0.17711E-38 c Velocity[Z] 0.12794E-38 c Pressure 0.45384E-18 0 0.10000E+01 -0.45384E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01181 0.89157 0.1418 0.1418 v Velocity[Y] -3.4886e-18 1.5875e-17 3.5539e-19 3.5539e-19 v Velocity[Z] -4.3351e-18 5.7273e-18 -8.1099e-22 -8.1099e-22 v ǁVelocityǁ 0.01181 0.89157 0.1418 0.1418 v Pressure 0 0 0 0 v CourantNb 0 3.2321e-16 1.9776e-17 1.9776e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.231000000E+02 TIME STEP NUMBER 231 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31294E-11 0.10413E+00 Friction velocity uk : 0.31294E-11 0.10413E+00 Dimensionless distance yplus : 0.15647E-08 0.10413E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42593E-02 1483 0.90294E-08 0.73337E-05 0.12970E+00 c Velocity[X] 0.73337E-05 c Velocity[Y] 0.17007E-38 c Velocity[Z] 0.24525E-38 c Pressure 0.45448E-18 0 0.10000E+01 -0.45448E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011784 0.89181 0.14189 0.14189 v Velocity[Y] -3.5065e-18 1.5856e-17 3.5442e-19 3.5442e-19 v Velocity[Z] -4.3299e-18 5.7429e-18 -3.3215e-22 -3.3215e-22 v ǁVelocityǁ 0.011784 0.89181 0.14189 0.14189 v Pressure 0 0 0 0 v CourantNb 0 3.2288e-16 1.9779e-17 1.9779e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.232000000E+02 TIME STEP NUMBER 232 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31222E-11 0.10401E+00 Friction velocity uk : 0.31222E-11 0.10401E+00 Dimensionless distance yplus : 0.15611E-08 0.10401E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42628E-02 1483 0.89932E-08 0.72849E-05 0.12916E+00 c Velocity[X] 0.72849E-05 c Velocity[Y] 0.17346E-38 c Velocity[Z] 0.17338E-38 c Pressure 0.45499E-18 0 0.10000E+01 -0.45499E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011757 0.89204 0.14198 0.14198 v Velocity[Y] -3.5273e-18 1.5838e-17 3.5345e-19 3.5345e-19 v Velocity[Z] -4.328e-18 5.7388e-18 -7.248e-22 -7.248e-22 v ǁVelocityǁ 0.011757 0.89204 0.14198 0.14198 v Pressure 0 0 0 0 v CourantNb 0 3.2267e-16 1.9804e-17 1.9804e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.233000000E+02 TIME STEP NUMBER 233 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31027E-11 0.10390E+00 Friction velocity uk : 0.31027E-11 0.10390E+00 Dimensionless distance yplus : 0.15513E-08 0.10390E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42664E-02 1482 0.90292E-08 0.72366E-05 0.12862E+00 c Velocity[X] 0.72366E-05 c Velocity[Y] 0.17140E-38 c Velocity[Z] 0.23739E-38 c Pressure 0.45548E-18 0 0.10000E+01 -0.45548E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011731 0.89228 0.14207 0.14207 v Velocity[Y] -3.5466e-18 1.5821e-17 3.5248e-19 3.5248e-19 v Velocity[Z] -4.366e-18 5.7419e-18 -3.1639e-22 -3.1639e-22 v ǁVelocityǁ 0.011731 0.89228 0.14207 0.14207 v Pressure 0 0 0 0 v CourantNb 0 3.2419e-16 1.9811e-17 1.9811e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.234000000E+02 TIME STEP NUMBER 234 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30894E-11 0.10379E+00 Friction velocity uk : 0.30894E-11 0.10379E+00 Dimensionless distance yplus : 0.15447E-08 0.10379E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42699E-02 1482 0.89933E-08 0.71888E-05 0.12808E+00 c Velocity[X] 0.71888E-05 c Velocity[Y] 0.20332E-38 c Velocity[Z] 0.21784E-38 c Pressure 0.45606E-18 0 0.10000E+01 -0.45606E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011704 0.89251 0.14216 0.14216 v Velocity[Y] -3.5671e-18 1.58e-17 3.515e-19 3.515e-19 v Velocity[Z] -4.3441e-18 5.7586e-18 -3.097e-22 -3.097e-22 v ǁVelocityǁ 0.011704 0.89251 0.14216 0.14216 v Pressure 0 0 0 0 v CourantNb 0 3.238e-16 1.9825e-17 1.9825e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.235000000E+02 TIME STEP NUMBER 235 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30824E-11 0.10368E+00 Friction velocity uk : 0.30824E-11 0.10368E+00 Dimensionless distance yplus : 0.15412E-08 0.10368E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42734E-02 1481 0.90296E-08 0.71415E-05 0.12755E+00 c Velocity[X] 0.71415E-05 c Velocity[Y] 0.19797E-38 c Velocity[Z] 0.22607E-38 c Pressure 0.45659E-18 0 0.10000E+01 -0.45659E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011678 0.89274 0.14225 0.14225 v Velocity[Y] -3.5861e-18 1.5775e-17 3.5051e-19 3.5051e-19 v Velocity[Z] -4.3539e-18 5.7536e-18 -2.7874e-22 -2.7874e-22 v ǁVelocityǁ 0.011678 0.89274 0.14225 0.14225 v Pressure 0 0 0 0 v CourantNb 0 3.244e-16 1.986e-17 1.986e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.236000000E+02 TIME STEP NUMBER 236 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30563E-11 0.10357E+00 Friction velocity uk : 0.30563E-11 0.10357E+00 Dimensionless distance yplus : 0.15281E-08 0.10357E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42769E-02 1481 0.89939E-08 0.70947E-05 0.12703E+00 c Velocity[X] 0.70947E-05 c Velocity[Y] 0.19217E-38 c Velocity[Z] 0.15391E-38 c Pressure 0.45713E-18 0 0.10000E+01 -0.45713E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011653 0.89297 0.14234 0.14234 v Velocity[Y] -3.605e-18 1.5755e-17 3.4952e-19 3.4952e-19 v Velocity[Z] -4.3468e-18 5.7481e-18 -2.5832e-22 -2.5832e-22 v ǁVelocityǁ 0.011653 0.89297 0.14234 0.14234 v Pressure 0 0 0 0 v CourantNb 0 3.2495e-16 1.9878e-17 1.9878e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.237000000E+02 TIME STEP NUMBER 237 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30837E-11 0.10346E+00 Friction velocity uk : 0.30837E-11 0.10346E+00 Dimensionless distance yplus : 0.15418E-08 0.10346E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42804E-02 1480 0.90306E-08 0.70485E-05 0.12651E+00 c Velocity[X] 0.70485E-05 c Velocity[Y] 0.17293E-38 c Velocity[Z] 0.15857E-38 c Pressure 0.45755E-18 0 0.10000E+01 -0.45755E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011627 0.89319 0.14243 0.14243 v Velocity[Y] -3.6247e-18 1.5735e-17 3.4853e-19 3.4853e-19 v Velocity[Z] -4.3546e-18 5.7523e-18 -9.7899e-22 -9.7899e-22 v ǁVelocityǁ 0.011627 0.89319 0.14243 0.14243 v Pressure 0 0 0 0 v CourantNb 0 3.2464e-16 1.9896e-17 1.9896e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.238000000E+02 TIME STEP NUMBER 238 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30176E-11 0.10335E+00 Friction velocity uk : 0.30176E-11 0.10335E+00 Dimensionless distance yplus : 0.15088E-08 0.10335E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42839E-02 1480 0.89952E-08 0.70027E-05 0.12599E+00 c Velocity[X] 0.70027E-05 c Velocity[Y] 0.18107E-38 c Velocity[Z] 0.18847E-38 c Pressure 0.45817E-18 0 0.10000E+01 -0.45817E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011601 0.89342 0.14252 0.14252 v Velocity[Y] -3.6439e-18 1.5715e-17 3.4753e-19 3.4753e-19 v Velocity[Z] -4.3626e-18 5.7685e-18 -5.3559e-22 -5.3559e-22 v ǁVelocityǁ 0.011601 0.89342 0.14252 0.14252 v Pressure 0 0 0 0 v CourantNb 0 3.2517e-16 1.9896e-17 1.9896e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.239000000E+02 TIME STEP NUMBER 239 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30397E-11 0.10324E+00 Friction velocity uk : 0.30397E-11 0.10324E+00 Dimensionless distance yplus : 0.15198E-08 0.10324E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42873E-02 1479 0.90321E-08 0.69574E-05 0.12548E+00 c Velocity[X] 0.69574E-05 c Velocity[Y] 0.18585E-38 c Velocity[Z] 0.24532E-38 c Pressure 0.45863E-18 0 0.10000E+01 -0.45863E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011576 0.89364 0.14261 0.14261 v Velocity[Y] -3.6628e-18 1.5696e-17 3.4652e-19 3.4652e-19 v Velocity[Z] -4.3159e-18 5.7561e-18 -6.9305e-22 -6.9305e-22 v ǁVelocityǁ 0.011576 0.89364 0.14261 0.14261 v Pressure 0 0 0 0 v CourantNb 0 3.2492e-16 1.9913e-17 1.9913e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.240000000E+02 TIME STEP NUMBER 240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30477E-11 0.10313E+00 Friction velocity uk : 0.30477E-11 0.10313E+00 Dimensionless distance yplus : 0.15239E-08 0.10313E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42908E-02 1479 0.89970E-08 0.69126E-05 0.12497E+00 c Velocity[X] 0.69126E-05 c Velocity[Y] 0.19154E-38 c Velocity[Z] 0.20588E-38 c Pressure 0.45917E-18 0 0.10000E+01 -0.45917E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011551 0.89387 0.1427 0.1427 v Velocity[Y] -3.683e-18 1.5674e-17 3.4551e-19 3.4551e-19 v Velocity[Z] -4.3547e-18 5.7498e-18 -3.694e-22 -3.694e-22 v ǁVelocityǁ 0.011551 0.89387 0.1427 0.1427 v Pressure 0 0 0 0 v CourantNb 0 3.2491e-16 1.9948e-17 1.9948e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.241000000E+02 TIME STEP NUMBER 241 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30047E-11 0.10302E+00 Friction velocity uk : 0.30047E-11 0.10302E+00 Dimensionless distance yplus : 0.15024E-08 0.10302E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42943E-02 1478 0.90342E-08 0.68683E-05 0.12446E+00 c Velocity[X] 0.68683E-05 c Velocity[Y] 0.18782E-38 c Velocity[Z] 0.21252E-38 c Pressure 0.45965E-18 0 0.10000E+01 -0.45965E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011525 0.89409 0.14279 0.14279 v Velocity[Y] -3.7018e-18 1.5657e-17 3.4449e-19 3.4449e-19 v Velocity[Z] -4.3497e-18 5.7617e-18 -5.1983e-22 -5.1983e-22 v ǁVelocityǁ 0.011525 0.89409 0.14279 0.14279 v Pressure 0 0 0 0 v CourantNb 0 3.2559e-16 1.9947e-17 1.9947e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.242000000E+02 TIME STEP NUMBER 242 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30002E-11 0.10291E+00 Friction velocity uk : 0.30002E-11 0.10291E+00 Dimensionless distance yplus : 0.15001E-08 0.10291E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.42977E-02 1478 0.89993E-08 0.68244E-05 0.12396E+00 c Velocity[X] 0.68244E-05 c Velocity[Y] 0.18784E-38 c Velocity[Z] 0.18009E-38 c Pressure 0.46009E-18 0 0.10000E+01 -0.46009E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011501 0.89431 0.14288 0.14288 v Velocity[Y] -3.7208e-18 1.5637e-17 3.4346e-19 3.4346e-19 v Velocity[Z] -4.3548e-18 5.7943e-18 -4.9706e-22 -4.9706e-22 v ǁVelocityǁ 0.011501 0.89431 0.14288 0.14288 v Pressure 0 0 0 0 v CourantNb 0 3.258e-16 1.998e-17 1.998e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.243000000E+02 TIME STEP NUMBER 243 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30061E-11 0.10281E+00 Friction velocity uk : 0.30061E-11 0.10281E+00 Dimensionless distance yplus : 0.15030E-08 0.10281E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43011E-02 1477 0.90368E-08 0.67810E-05 0.12347E+00 c Velocity[X] 0.67810E-05 c Velocity[Y] 0.17562E-38 c Velocity[Z] 0.15919E-38 c Pressure 0.46060E-18 0 0.10000E+01 -0.46060E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011476 0.89452 0.14296 0.14296 v Velocity[Y] -3.7405e-18 1.5618e-17 3.4243e-19 3.4243e-19 v Velocity[Z] -4.3544e-18 5.7695e-18 -9.049e-22 -9.049e-22 v ǁVelocityǁ 0.011476 0.89452 0.14296 0.14296 v Pressure 0 0 0 0 v CourantNb 0 3.2597e-16 1.9999e-17 1.9999e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.244000000E+02 TIME STEP NUMBER 244 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30262E-11 0.10270E+00 Friction velocity uk : 0.30262E-11 0.10270E+00 Dimensionless distance yplus : 0.15131E-08 0.10270E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43045E-02 1477 0.90022E-08 0.67381E-05 0.12297E+00 c Velocity[X] 0.67381E-05 c Velocity[Y] 0.16960E-38 c Velocity[Z] 0.18906E-38 c Pressure 0.46106E-18 0 0.10000E+01 -0.46106E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011451 0.89474 0.14305 0.14305 v Velocity[Y] -3.7602e-18 1.5602e-17 3.414e-19 3.414e-19 v Velocity[Z] -4.3887e-18 5.7455e-18 -1.2087e-21 -1.2087e-21 v ǁVelocityǁ 0.011451 0.89474 0.14305 0.14305 v Pressure 0 0 0 0 v CourantNb 0 3.2634e-16 2.0007e-17 2.0007e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.245000000E+02 TIME STEP NUMBER 245 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30042E-11 0.10260E+00 Friction velocity uk : 0.30042E-11 0.10260E+00 Dimensionless distance yplus : 0.15021E-08 0.10260E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43079E-02 1476 0.90399E-08 0.66956E-05 0.12249E+00 c Velocity[X] 0.66956E-05 c Velocity[Y] 0.19391E-38 c Velocity[Z] 0.15259E-38 c Pressure 0.46164E-18 0 0.10000E+01 -0.46164E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011427 0.89496 0.14314 0.14314 v Velocity[Y] -3.779e-18 1.5581e-17 3.4035e-19 3.4035e-19 v Velocity[Z] -4.3773e-18 5.7838e-18 -1.0002e-21 -1.0002e-21 v ǁVelocityǁ 0.011427 0.89496 0.14314 0.14314 v Pressure 0 0 0 0 v CourantNb 0 3.2731e-16 2.0042e-17 2.0042e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.246000000E+02 TIME STEP NUMBER 246 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29769E-11 0.10249E+00 Friction velocity uk : 0.29769E-11 0.10249E+00 Dimensionless distance yplus : 0.14884E-08 0.10249E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43113E-02 1476 0.90056E-08 0.66535E-05 0.12200E+00 c Velocity[X] 0.66535E-05 c Velocity[Y] 0.14884E-38 c Velocity[Z] 0.24425E-38 c Pressure 0.46226E-18 0 0.10000E+01 -0.46226E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011402 0.89517 0.14323 0.14323 v Velocity[Y] -3.7988e-18 1.5567e-17 3.3931e-19 3.3931e-19 v Velocity[Z] -4.346e-18 5.7954e-18 -6.7338e-22 -6.7338e-22 v ǁVelocityǁ 0.011402 0.89517 0.14323 0.14323 v Pressure 0 0 0 0 v CourantNb 0 3.272e-16 2.0065e-17 2.0065e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.247000000E+02 TIME STEP NUMBER 247 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29499E-11 0.10239E+00 Friction velocity uk : 0.29499E-11 0.10239E+00 Dimensionless distance yplus : 0.14750E-08 0.10239E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43147E-02 1476 0.89715E-08 0.66119E-05 0.12152E+00 c Velocity[X] 0.66119E-05 c Velocity[Y] 0.16818E-38 c Velocity[Z] 0.27129E-38 c Pressure 0.46285E-18 0 0.10000E+01 -0.46285E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011378 0.89538 0.14332 0.14332 v Velocity[Y] -3.8184e-18 1.5549e-17 3.3826e-19 3.3826e-19 v Velocity[Z] -4.4024e-18 5.776e-18 -5.8061e-22 -5.8061e-22 v ǁVelocityǁ 0.011378 0.89538 0.14332 0.14332 v Pressure 0 0 0 0 v CourantNb 0 3.261e-16 2.008e-17 2.008e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.248000000E+02 TIME STEP NUMBER 248 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29553E-11 0.10228E+00 Friction velocity uk : 0.29553E-11 0.10228E+00 Dimensionless distance yplus : 0.14777E-08 0.10228E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43181E-02 1475 0.90096E-08 0.65706E-05 0.12104E+00 c Velocity[X] 0.65706E-05 c Velocity[Y] 0.15030E-38 c Velocity[Z] 0.27197E-38 c Pressure 0.46325E-18 0 0.10000E+01 -0.46325E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011354 0.8956 0.1434 0.1434 v Velocity[Y] -3.8379e-18 1.5535e-17 3.3721e-19 3.3721e-19 v Velocity[Z] -4.3778e-18 5.8027e-18 -5.3163e-22 -5.3163e-22 v ǁVelocityǁ 0.011354 0.8956 0.1434 0.1434 v Pressure 0 0 0 0 v CourantNb 0 3.286e-16 2.0083e-17 2.0083e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.249000000E+02 TIME STEP NUMBER 249 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29162E-11 0.10218E+00 Friction velocity uk : 0.29162E-11 0.10218E+00 Dimensionless distance yplus : 0.14581E-08 0.10218E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43215E-02 1475 0.89757E-08 0.65299E-05 0.12057E+00 c Velocity[X] 0.65299E-05 c Velocity[Y] 0.17039E-38 c Velocity[Z] 0.15582E-38 c Pressure 0.46377E-18 0 0.10000E+01 -0.46377E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01133 0.89581 0.14349 0.14349 v Velocity[Y] -3.8579e-18 1.5519e-17 3.3616e-19 3.3616e-19 v Velocity[Z] -4.3791e-18 5.7986e-18 -5.6917e-22 -5.6917e-22 v ǁVelocityǁ 0.01133 0.89581 0.14349 0.14349 v Pressure 0 0 0 0 v CourantNb 0 3.2743e-16 2.0121e-17 2.0121e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.250000000E+02 TIME STEP NUMBER 250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29339E-11 0.10208E+00 Friction velocity uk : 0.29339E-11 0.10208E+00 Dimensionless distance yplus : 0.14669E-08 0.10208E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43248E-02 1474 0.90140E-08 0.64895E-05 0.12010E+00 c Velocity[X] 0.64895E-05 c Velocity[Y] 0.18279E-38 c Velocity[Z] 0.15903E-38 c Pressure 0.46419E-18 0 0.10000E+01 -0.46419E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011307 0.89601 0.14358 0.14358 v Velocity[Y] -3.8773e-18 1.55e-17 3.351e-19 3.351e-19 v Velocity[Z] -4.391e-18 5.7956e-18 -6.7605e-22 -6.7605e-22 v ǁVelocityǁ 0.011307 0.89601 0.14358 0.14358 v Pressure 0 0 0 0 v CourantNb 0 3.2855e-16 2.0143e-17 2.0143e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.251000000E+02 TIME STEP NUMBER 251 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29216E-11 0.10197E+00 Friction velocity uk : 0.29216E-11 0.10197E+00 Dimensionless distance yplus : 0.14608E-08 0.10197E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43282E-02 1474 0.89804E-08 0.64495E-05 0.11964E+00 c Velocity[X] 0.64495E-05 c Velocity[Y] 0.16665E-38 c Velocity[Z] 0.17122E-38 c Pressure 0.46481E-18 0 0.10000E+01 -0.46481E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011283 0.89622 0.14366 0.14366 v Velocity[Y] -3.8976e-18 1.5482e-17 3.3403e-19 3.3403e-19 v Velocity[Z] -4.3823e-18 5.7917e-18 -1.0174e-21 -1.0174e-21 v ǁVelocityǁ 0.011283 0.89622 0.14366 0.14366 v Pressure 0 0 0 0 v CourantNb 0 3.2771e-16 2.0152e-17 2.0152e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.252000000E+02 TIME STEP NUMBER 252 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28809E-11 0.10187E+00 Friction velocity uk : 0.28809E-11 0.10187E+00 Dimensionless distance yplus : 0.14405E-08 0.10187E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43315E-02 1473 0.90190E-08 0.64100E-05 0.11917E+00 c Velocity[X] 0.64100E-05 c Velocity[Y] 0.18855E-38 c Velocity[Z] 0.25573E-38 c Pressure 0.46514E-18 0 0.10000E+01 -0.46514E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01126 0.89643 0.14375 0.14375 v Velocity[Y] -3.9175e-18 1.5464e-17 3.3296e-19 3.3296e-19 v Velocity[Z] -4.4019e-18 5.7891e-18 -8.0176e-22 -8.0176e-22 v ǁVelocityǁ 0.01126 0.89643 0.14375 0.14375 v Pressure 0 0 0 0 v CourantNb 0 3.2784e-16 2.0161e-17 2.0161e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.253000000E+02 TIME STEP NUMBER 253 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28689E-11 0.10177E+00 Friction velocity uk : 0.28689E-11 0.10177E+00 Dimensionless distance yplus : 0.14344E-08 0.10177E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43348E-02 1473 0.89856E-08 0.63708E-05 0.11871E+00 c Velocity[X] 0.63708E-05 c Velocity[Y] 0.15971E-38 c Velocity[Z] 0.13422E-38 c Pressure 0.46570E-18 0 0.10000E+01 -0.46570E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011236 0.89663 0.14384 0.14384 v Velocity[Y] -3.9371e-18 1.5447e-17 3.3189e-19 3.3189e-19 v Velocity[Z] -4.3998e-18 5.805e-18 -7.0892e-22 -7.0892e-22 v ǁVelocityǁ 0.011236 0.89663 0.14384 0.14384 v Pressure 0 0 0 0 v CourantNb 0 3.2894e-16 2.0199e-17 2.0199e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.254000000E+02 TIME STEP NUMBER 254 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28524E-11 0.10167E+00 Friction velocity uk : 0.28524E-11 0.10167E+00 Dimensionless distance yplus : 0.14262E-08 0.10167E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43381E-02 1472 0.90245E-08 0.63320E-05 0.11826E+00 c Velocity[X] 0.63320E-05 c Velocity[Y] 0.18109E-38 c Velocity[Z] 0.22644E-38 c Pressure 0.46625E-18 0 0.10000E+01 -0.46625E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011213 0.89684 0.14392 0.14392 v Velocity[Y] -3.9574e-18 1.5429e-17 3.3082e-19 3.3082e-19 v Velocity[Z] -4.406e-18 5.8104e-18 -6.738e-22 -6.738e-22 v ǁVelocityǁ 0.011213 0.89684 0.14392 0.14392 v Pressure 0 0 0 0 v CourantNb 0 3.2939e-16 2.0227e-17 2.0227e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.255000000E+02 TIME STEP NUMBER 255 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28655E-11 0.10157E+00 Friction velocity uk : 0.28655E-11 0.10157E+00 Dimensionless distance yplus : 0.14327E-08 0.10157E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43414E-02 1472 0.89913E-08 0.62936E-05 0.11781E+00 c Velocity[X] 0.62936E-05 c Velocity[Y] 0.19028E-38 c Velocity[Z] 0.21625E-38 c Pressure 0.46674E-18 0 0.10000E+01 -0.46674E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01119 0.89704 0.14401 0.14401 v Velocity[Y] -3.9772e-18 1.541e-17 3.2973e-19 3.2973e-19 v Velocity[Z] -4.3966e-18 5.8053e-18 -4.9955e-22 -4.9955e-22 v ǁVelocityǁ 0.01119 0.89704 0.14401 0.14401 v Pressure 0 0 0 0 v CourantNb 0 3.29e-16 2.0213e-17 2.0213e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.256000000E+02 TIME STEP NUMBER 256 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28042E-11 0.10147E+00 Friction velocity uk : 0.28042E-11 0.10147E+00 Dimensionless distance yplus : 0.14021E-08 0.10147E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43447E-02 1471 0.90305E-08 0.62556E-05 0.11736E+00 c Velocity[X] 0.62556E-05 c Velocity[Y] 0.19767E-38 c Velocity[Z] 0.12471E-38 c Pressure 0.46723E-18 0 0.10000E+01 -0.46723E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011167 0.89724 0.14409 0.14409 v Velocity[Y] -3.998e-18 1.5391e-17 3.2865e-19 3.2865e-19 v Velocity[Z] -4.4195e-18 5.8015e-18 -6.1776e-22 -6.1776e-22 v ǁVelocityǁ 0.011167 0.89724 0.14409 0.14409 v Pressure 0 0 0 0 v CourantNb 0 3.2914e-16 2.0243e-17 2.0243e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.257000000E+02 TIME STEP NUMBER 257 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28345E-11 0.10137E+00 Friction velocity uk : 0.28345E-11 0.10137E+00 Dimensionless distance yplus : 0.14172E-08 0.10137E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43480E-02 1471 0.89975E-08 0.62180E-05 0.11691E+00 c Velocity[X] 0.62180E-05 c Velocity[Y] 0.17389E-38 c Velocity[Z] 0.11833E-38 c Pressure 0.46766E-18 0 0.10000E+01 -0.46766E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011145 0.89744 0.14418 0.14418 v Velocity[Y] -4.0172e-18 1.5372e-17 3.2755e-19 3.2755e-19 v Velocity[Z] -4.4011e-18 5.7943e-18 -5.9708e-22 -5.9708e-22 v ǁVelocityǁ 0.011145 0.89744 0.14418 0.14418 v Pressure 0 0 0 0 v CourantNb 0 3.2993e-16 2.0261e-17 2.0261e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.258000000E+02 TIME STEP NUMBER 258 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28321E-11 0.10127E+00 Friction velocity uk : 0.28321E-11 0.10127E+00 Dimensionless distance yplus : 0.14161E-08 0.10127E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43513E-02 1470 0.90369E-08 0.61807E-05 0.11647E+00 c Velocity[X] 0.61807E-05 c Velocity[Y] 0.17879E-38 c Velocity[Z] 0.21430E-38 c Pressure 0.46824E-18 0 0.10000E+01 -0.46824E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011122 0.89764 0.14427 0.14427 v Velocity[Y] -4.0363e-18 1.5354e-17 3.2646e-19 3.2646e-19 v Velocity[Z] -4.4209e-18 5.829e-18 -8.1409e-22 -8.1409e-22 v ǁVelocityǁ 0.011122 0.89764 0.14427 0.14427 v Pressure 0 0 0 0 v CourantNb 0 3.2957e-16 2.0262e-17 2.0262e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.259000000E+02 TIME STEP NUMBER 259 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28362E-11 0.10117E+00 Friction velocity uk : 0.28362E-11 0.10117E+00 Dimensionless distance yplus : 0.14181E-08 0.10117E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43546E-02 1470 0.90042E-08 0.61438E-05 0.11604E+00 c Velocity[X] 0.61438E-05 c Velocity[Y] 0.16984E-38 c Velocity[Z] 0.20764E-38 c Pressure 0.46866E-18 0 0.10000E+01 -0.46866E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0111 0.89784 0.14435 0.14435 v Velocity[Y] -4.056e-18 1.5336e-17 3.2535e-19 3.2535e-19 v Velocity[Z] -4.3882e-18 5.8082e-18 -4.5687e-22 -4.5687e-22 v ǁVelocityǁ 0.0111 0.89784 0.14435 0.14435 v Pressure 0 0 0 0 v CourantNb 0 3.2982e-16 2.0298e-17 2.0298e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.260000000E+02 TIME STEP NUMBER 260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27737E-11 0.10108E+00 Friction velocity uk : 0.27737E-11 0.10108E+00 Dimensionless distance yplus : 0.13868E-08 0.10108E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43578E-02 1470 0.89718E-08 0.61073E-05 0.11560E+00 c Velocity[X] 0.61073E-05 c Velocity[Y] 0.19080E-38 c Velocity[Z] 0.17822E-38 c Pressure 0.46903E-18 0 0.10000E+01 -0.46903E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011077 0.89803 0.14444 0.14444 v Velocity[Y] -4.0752e-18 1.5316e-17 3.2425e-19 3.2425e-19 v Velocity[Z] -4.3897e-18 5.816e-18 -1.8797e-22 -1.8797e-22 v ǁVelocityǁ 0.011077 0.89803 0.14444 0.14444 v Pressure 0 0 0 0 v CourantNb 0 3.2915e-16 2.0296e-17 2.0296e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.261000000E+02 TIME STEP NUMBER 261 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28024E-11 0.10098E+00 Friction velocity uk : 0.28024E-11 0.10098E+00 Dimensionless distance yplus : 0.14012E-08 0.10098E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43611E-02 1469 0.90114E-08 0.60711E-05 0.11517E+00 c Velocity[X] 0.60711E-05 c Velocity[Y] 0.17404E-38 c Velocity[Z] 0.17331E-38 c Pressure 0.46958E-18 0 0.10000E+01 -0.46958E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011055 0.89823 0.14452 0.14452 v Velocity[Y] -4.094e-18 1.5298e-17 3.2314e-19 3.2314e-19 v Velocity[Z] -4.4125e-18 5.8095e-18 -2.7046e-22 -2.7046e-22 v ǁVelocityǁ 0.011055 0.89823 0.14452 0.14452 v Pressure 0 0 0 0 v CourantNb 0 3.2995e-16 2.0308e-17 2.0308e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.262000000E+02 TIME STEP NUMBER 262 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26693E-11 0.10088E+00 Friction velocity uk : 0.26693E-11 0.10088E+00 Dimensionless distance yplus : 0.13346E-08 0.10088E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43643E-02 1469 0.89792E-08 0.60353E-05 0.11474E+00 c Velocity[X] 0.60353E-05 c Velocity[Y] 0.21109E-38 c Velocity[Z] 0.18723E-38 c Pressure 0.47009E-18 0 0.10000E+01 -0.47009E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011033 0.89842 0.14461 0.14461 v Velocity[Y] -4.1156e-18 1.5278e-17 3.2202e-19 3.2202e-19 v Velocity[Z] -4.3926e-18 5.8236e-18 -6.7088e-22 -6.7088e-22 v ǁVelocityǁ 0.011033 0.89842 0.14461 0.14461 v Pressure 0 0 0 0 v CourantNb 0 3.3024e-16 2.0313e-17 2.0313e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.263000000E+02 TIME STEP NUMBER 263 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28056E-11 0.10079E+00 Friction velocity uk : 0.28056E-11 0.10079E+00 Dimensionless distance yplus : 0.14028E-08 0.10079E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43675E-02 1468 0.90190E-08 0.59998E-05 0.11432E+00 c Velocity[X] 0.59998E-05 c Velocity[Y] 0.19573E-38 c Velocity[Z] 0.15210E-38 c Pressure 0.47042E-18 0 0.10000E+01 -0.47042E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011011 0.89862 0.14469 0.14469 v Velocity[Y] -4.1349e-18 1.5258e-17 3.2089e-19 3.2089e-19 v Velocity[Z] -4.3773e-18 5.8089e-18 -7.099e-22 -7.099e-22 v ǁVelocityǁ 0.011011 0.89862 0.14469 0.14469 v Pressure 0 0 0 0 v CourantNb 0 3.2879e-16 2.0334e-17 2.0334e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.264000000E+02 TIME STEP NUMBER 264 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27617E-11 0.10069E+00 Friction velocity uk : 0.27617E-11 0.10069E+00 Dimensionless distance yplus : 0.13808E-08 0.10069E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43707E-02 1468 0.89870E-08 0.59647E-05 0.11389E+00 c Velocity[X] 0.59647E-05 c Velocity[Y] 0.19450E-38 c Velocity[Z] 0.27401E-38 c Pressure 0.47111E-18 0 0.10000E+01 -0.47111E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010989 0.89881 0.14477 0.14477 v Velocity[Y] -4.1546e-18 1.5241e-17 3.1976e-19 3.1976e-19 v Velocity[Z] -4.406e-18 5.8184e-18 -5.8172e-22 -5.8172e-22 v ǁVelocityǁ 0.010989 0.89881 0.14477 0.14477 v Pressure 0 0 0 0 v CourantNb 0 3.2961e-16 2.0347e-17 2.0347e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.265000000E+02 TIME STEP NUMBER 265 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27406E-11 0.10059E+00 Friction velocity uk : 0.27406E-11 0.10059E+00 Dimensionless distance yplus : 0.13703E-08 0.10059E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43740E-02 1467 0.90272E-08 0.59298E-05 0.11348E+00 c Velocity[X] 0.59298E-05 c Velocity[Y] 0.18581E-38 c Velocity[Z] 0.36418E-38 c Pressure 0.47161E-18 0 0.10000E+01 -0.47161E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010968 0.899 0.14486 0.14486 v Velocity[Y] -4.1738e-18 1.5219e-17 3.1862e-19 3.1862e-19 v Velocity[Z] -4.4453e-18 5.8445e-18 -9.2085e-22 -9.2085e-22 v ǁVelocityǁ 0.010968 0.899 0.14486 0.14486 v Pressure 0 0 0 0 v CourantNb 0 3.3069e-16 2.0385e-17 2.0385e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.266000000E+02 TIME STEP NUMBER 266 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27808E-11 0.10050E+00 Friction velocity uk : 0.27808E-11 0.10050E+00 Dimensionless distance yplus : 0.13904E-08 0.10050E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43772E-02 1467 0.89953E-08 0.58954E-05 0.11306E+00 c Velocity[X] 0.58954E-05 c Velocity[Y] 0.19760E-38 c Velocity[Z] 0.26651E-38 c Pressure 0.47197E-18 0 0.10000E+01 -0.47197E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010946 0.89919 0.14494 0.14494 v Velocity[Y] -4.1942e-18 1.52e-17 3.1748e-19 3.1748e-19 v Velocity[Z] -4.4141e-18 5.8078e-18 -6.5359e-22 -6.5359e-22 v ǁVelocityǁ 0.010946 0.89919 0.14494 0.14494 v Pressure 0 0 0 0 v CourantNb 0 3.3161e-16 2.0412e-17 2.0412e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.267000000E+02 TIME STEP NUMBER 267 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26921E-11 0.10040E+00 Friction velocity uk : 0.26921E-11 0.10040E+00 Dimensionless distance yplus : 0.13461E-08 0.10040E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43803E-02 1466 0.90357E-08 0.58612E-05 0.11265E+00 c Velocity[X] 0.58612E-05 c Velocity[Y] 0.18636E-38 c Velocity[Z] 0.22010E-38 c Pressure 0.47253E-18 0 0.10000E+01 -0.47253E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010925 0.89938 0.14503 0.14503 v Velocity[Y] -4.2131e-18 1.5181e-17 3.1633e-19 3.1633e-19 v Velocity[Z] -4.4159e-18 5.8307e-18 -6.6345e-22 -6.6345e-22 v ǁVelocityǁ 0.010925 0.89938 0.14503 0.14503 v Pressure 0 0 0 0 v CourantNb 0 3.3134e-16 2.0431e-17 2.0431e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.268000000E+02 TIME STEP NUMBER 268 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27508E-11 0.10031E+00 Friction velocity uk : 0.27508E-11 0.10031E+00 Dimensionless distance yplus : 0.13754E-08 0.10031E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43835E-02 1466 0.90041E-08 0.58274E-05 0.11224E+00 c Velocity[X] 0.58274E-05 c Velocity[Y] 0.19122E-38 c Velocity[Z] 0.17206E-38 c Pressure 0.47294E-18 0 0.10000E+01 -0.47294E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010903 0.89956 0.14511 0.14511 v Velocity[Y] -4.2328e-18 1.516e-17 3.1518e-19 3.1518e-19 v Velocity[Z] -4.4325e-18 5.8291e-18 -7.6901e-22 -7.6901e-22 v ǁVelocityǁ 0.010903 0.89956 0.14511 0.14511 v Pressure 0 0 0 0 v CourantNb 0 3.3136e-16 2.0462e-17 2.0462e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.269000000E+02 TIME STEP NUMBER 269 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27686E-11 0.10022E+00 Friction velocity uk : 0.27686E-11 0.10022E+00 Dimensionless distance yplus : 0.13843E-08 0.10022E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43867E-02 1466 0.89727E-08 0.57939E-05 0.11183E+00 c Velocity[X] 0.57939E-05 c Velocity[Y] 0.19723E-38 c Velocity[Z] 0.17056E-38 c Pressure 0.47337E-18 0 0.10000E+01 -0.47337E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010882 0.89975 0.14519 0.14519 v Velocity[Y] -4.2529e-18 1.5141e-17 3.1403e-19 3.1403e-19 v Velocity[Z] -4.4387e-18 5.8192e-18 -8.452e-22 -8.452e-22 v ǁVelocityǁ 0.010882 0.89975 0.14519 0.14519 v Pressure 0 0 0 0 v CourantNb 0 3.328e-16 2.0473e-17 2.0473e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.270000000E+02 TIME STEP NUMBER 270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25975E-11 0.10012E+00 Friction velocity uk : 0.25975E-11 0.10012E+00 Dimensionless distance yplus : 0.12987E-08 0.10012E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43899E-02 1465 0.90133E-08 0.57607E-05 0.11143E+00 c Velocity[X] 0.57607E-05 c Velocity[Y] 0.20121E-38 c Velocity[Z] 0.15951E-38 c Pressure 0.47392E-18 0 0.10000E+01 -0.47392E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010861 0.89994 0.14528 0.14528 v Velocity[Y] -4.2733e-18 1.512e-17 3.1287e-19 3.1287e-19 v Velocity[Z] -4.4211e-18 5.8234e-18 -8.7887e-22 -8.7887e-22 v ǁVelocityǁ 0.010861 0.89994 0.14528 0.14528 v Pressure 0 0 0 0 v CourantNb 0 3.3227e-16 2.0485e-17 2.0485e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.271000000E+02 TIME STEP NUMBER 271 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27668E-11 0.10003E+00 Friction velocity uk : 0.27668E-11 0.10003E+00 Dimensionless distance yplus : 0.13834E-08 0.10003E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43930E-02 1465 0.89821E-08 0.57278E-05 0.11103E+00 c Velocity[X] 0.57278E-05 c Velocity[Y] 0.17915E-38 c Velocity[Z] 0.16898E-38 c Pressure 0.47430E-18 0 0.10000E+01 -0.47430E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01084 0.90012 0.14536 0.14536 v Velocity[Y] -4.2921e-18 1.51e-17 3.117e-19 3.117e-19 v Velocity[Z] -4.4098e-18 5.8271e-18 -7.5712e-22 -7.5712e-22 v ǁVelocityǁ 0.01084 0.90012 0.14536 0.14536 v Pressure 0 0 0 0 v CourantNb 0 3.3189e-16 2.0506e-17 2.0506e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.272000000E+02 TIME STEP NUMBER 272 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27711E-11 0.99940E-01 Friction velocity uk : 0.27711E-11 0.99940E-01 Dimensionless distance yplus : 0.13856E-08 0.99940E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43962E-02 1464 0.90230E-08 0.56953E-05 0.11063E+00 c Velocity[X] 0.56953E-05 c Velocity[Y] 0.17592E-38 c Velocity[Z] 0.24328E-38 c Pressure 0.47477E-18 0 0.10000E+01 -0.47477E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010819 0.9003 0.14544 0.14544 v Velocity[Y] -4.3128e-18 1.5082e-17 3.1054e-19 3.1054e-19 v Velocity[Z] -4.4446e-18 5.8345e-18 -9.8233e-22 -9.8233e-22 v ǁVelocityǁ 0.010819 0.9003 0.14544 0.14544 v Pressure 0 0 0 0 v CourantNb 0 3.3076e-16 2.0514e-17 2.0514e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.273000000E+02 TIME STEP NUMBER 273 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26312E-11 0.99848E-01 Friction velocity uk : 0.26312E-11 0.99848E-01 Dimensionless distance yplus : 0.13156E-08 0.99848E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.43993E-02 1464 0.89919E-08 0.56630E-05 0.11023E+00 c Velocity[X] 0.56630E-05 c Velocity[Y] 0.14815E-38 c Velocity[Z] 0.32666E-38 c Pressure 0.47550E-18 0 0.10000E+01 -0.47550E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010799 0.90049 0.14553 0.14553 v Velocity[Y] -4.3328e-18 1.5072e-17 3.0938e-19 3.0938e-19 v Velocity[Z] -4.4387e-18 5.8863e-18 -5.0318e-22 -5.0318e-22 v ǁVelocityǁ 0.010799 0.90049 0.14553 0.14553 v Pressure 0 0 0 0 v CourantNb 0 3.3199e-16 2.0546e-17 2.0546e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.274000000E+02 TIME STEP NUMBER 274 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25329E-11 0.99757E-01 Friction velocity uk : 0.25329E-11 0.99757E-01 Dimensionless distance yplus : 0.12664E-08 0.99757E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44025E-02 1463 0.90331E-08 0.56310E-05 0.10984E+00 c Velocity[X] 0.56310E-05 c Velocity[Y] 0.15192E-38 c Velocity[Z] 0.25186E-38 c Pressure 0.47592E-18 0 0.10000E+01 -0.47592E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010778 0.90067 0.14561 0.14561 v Velocity[Y] -4.3522e-18 1.5057e-17 3.0822e-19 3.0822e-19 v Velocity[Z] -4.4694e-18 5.875e-18 -8.1229e-22 -8.1229e-22 v ǁVelocityǁ 0.010778 0.90067 0.14561 0.14561 v Pressure 0 0 0 0 v CourantNb 0 3.3328e-16 2.0588e-17 2.0588e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.275000000E+02 TIME STEP NUMBER 275 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25342E-11 0.99666E-01 Friction velocity uk : 0.25342E-11 0.99666E-01 Dimensionless distance yplus : 0.12671E-08 0.99666E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44056E-02 1463 0.90022E-08 0.55994E-05 0.10945E+00 c Velocity[X] 0.55994E-05 c Velocity[Y] 0.14758E-38 c Velocity[Z] 0.16494E-38 c Pressure 0.47634E-18 0 0.10000E+01 -0.47634E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010758 0.90085 0.14569 0.14569 v Velocity[Y] -4.3722e-18 1.5042e-17 3.0706e-19 3.0706e-19 v Velocity[Z] -4.4379e-18 5.8975e-18 -5.3729e-22 -5.3729e-22 v ǁVelocityǁ 0.010758 0.90085 0.14569 0.14569 v Pressure 0 0 0 0 v CourantNb 0 3.3373e-16 2.0618e-17 2.0618e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.276000000E+02 TIME STEP NUMBER 276 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27732E-11 0.99576E-01 Friction velocity uk : 0.27732E-11 0.99576E-01 Dimensionless distance yplus : 0.13866E-08 0.99576E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44087E-02 1463 0.89716E-08 0.55680E-05 0.10907E+00 c Velocity[X] 0.55680E-05 c Velocity[Y] 0.15520E-38 c Velocity[Z] 0.17986E-38 c Pressure 0.47683E-18 0 0.10000E+01 -0.47683E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010737 0.90103 0.14577 0.14577 v Velocity[Y] -4.3921e-18 1.5026e-17 3.059e-19 3.059e-19 v Velocity[Z] -4.4286e-18 5.8801e-18 -6.4473e-22 -6.4473e-22 v ǁVelocityǁ 0.010737 0.90103 0.14577 0.14577 v Pressure 0 0 0 0 v CourantNb 0 3.3284e-16 2.0634e-17 2.0634e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.277000000E+02 TIME STEP NUMBER 277 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24588E-11 0.99486E-01 Friction velocity uk : 0.24588E-11 0.99486E-01 Dimensionless distance yplus : 0.12294E-08 0.99486E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44118E-02 1462 0.90130E-08 0.55369E-05 0.10868E+00 c Velocity[X] 0.55369E-05 c Velocity[Y] 0.16854E-38 c Velocity[Z] 0.26818E-38 c Pressure 0.47720E-18 0 0.10000E+01 -0.47720E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010717 0.9012 0.14586 0.14586 v Velocity[Y] -4.4123e-18 1.501e-17 3.0474e-19 3.0474e-19 v Velocity[Z] -4.4384e-18 5.8804e-18 -7.5181e-22 -7.5181e-22 v ǁVelocityǁ 0.010717 0.9012 0.14586 0.14586 v Pressure 0 0 0 0 v CourantNb 0 3.3288e-16 2.0622e-17 2.0622e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.278000000E+02 TIME STEP NUMBER 278 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24423E-11 0.99396E-01 Friction velocity uk : 0.24423E-11 0.99396E-01 Dimensionless distance yplus : 0.12211E-08 0.99396E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44149E-02 1462 0.89825E-08 0.55061E-05 0.10830E+00 c Velocity[X] 0.55061E-05 c Velocity[Y] 0.16935E-38 c Velocity[Z] 0.34280E-38 c Pressure 0.47778E-18 0 0.10000E+01 -0.47778E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010697 0.90138 0.14594 0.14594 v Velocity[Y] -4.432e-18 1.4994e-17 3.0358e-19 3.0358e-19 v Velocity[Z] -4.4385e-18 5.9008e-18 -6.0957e-22 -6.0957e-22 v ǁVelocityǁ 0.010697 0.90138 0.14594 0.14594 v Pressure 0 0 0 0 v CourantNb 0 3.3259e-16 2.0659e-17 2.0659e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.279000000E+02 TIME STEP NUMBER 279 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24456E-11 0.99307E-01 Friction velocity uk : 0.24456E-11 0.99307E-01 Dimensionless distance yplus : 0.12228E-08 0.99307E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44180E-02 1461 0.90241E-08 0.54756E-05 0.10792E+00 c Velocity[X] 0.54756E-05 c Velocity[Y] 0.16271E-38 c Velocity[Z] 0.24214E-38 c Pressure 0.47816E-18 0 0.10000E+01 -0.47816E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010677 0.90156 0.14602 0.14602 v Velocity[Y] -4.451e-18 1.4977e-17 3.0242e-19 3.0242e-19 v Velocity[Z] -4.4359e-18 5.8872e-18 -6.4539e-22 -6.4539e-22 v ǁVelocityǁ 0.010677 0.90156 0.14602 0.14602 v Pressure 0 0 0 0 v CourantNb 0 3.3345e-16 2.0671e-17 2.0671e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.280000000E+02 TIME STEP NUMBER 280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27603E-11 0.99218E-01 Friction velocity uk : 0.27603E-11 0.99218E-01 Dimensionless distance yplus : 0.13801E-08 0.99218E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44211E-02 1461 0.89938E-08 0.54453E-05 0.10755E+00 c Velocity[X] 0.54453E-05 c Velocity[Y] 0.15055E-38 c Velocity[Z] 0.20775E-38 c Pressure 0.47852E-18 0 0.10000E+01 -0.47852E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010657 0.90173 0.1461 0.1461 v Velocity[Y] -4.4703e-18 1.4962e-17 3.0126e-19 3.0126e-19 v Velocity[Z] -4.4367e-18 5.8661e-18 -5.0715e-22 -5.0715e-22 v ǁVelocityǁ 0.010657 0.90173 0.1461 0.1461 v Pressure 0 0 0 0 v CourantNb 0 3.3304e-16 2.0692e-17 2.0692e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.281000000E+02 TIME STEP NUMBER 281 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23756E-11 0.99130E-01 Friction velocity uk : 0.23756E-11 0.99130E-01 Dimensionless distance yplus : 0.11878E-08 0.99130E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44241E-02 1460 0.90357E-08 0.54153E-05 0.10717E+00 c Velocity[X] 0.54153E-05 c Velocity[Y] 0.15861E-38 c Velocity[Z] 0.29951E-38 c Pressure 0.47906E-18 0 0.10000E+01 -0.47906E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010637 0.90191 0.14618 0.14618 v Velocity[Y] -4.4894e-18 1.4944e-17 3.0009e-19 3.0009e-19 v Velocity[Z] -4.4309e-18 5.8875e-18 2.3126e-22 2.3126e-22 v ǁVelocityǁ 0.010637 0.90191 0.14618 0.14618 v Pressure 0 0 0 0 v CourantNb 0 3.3256e-16 2.0694e-17 2.0694e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.282000000E+02 TIME STEP NUMBER 282 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21559E-11 0.99042E-01 Friction velocity uk : 0.21559E-11 0.99042E-01 Dimensionless distance yplus : 0.10779E-08 0.99042E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44272E-02 1460 0.90056E-08 0.53856E-05 0.10680E+00 c Velocity[X] 0.53856E-05 c Velocity[Y] 0.15597E-38 c Velocity[Z] 0.12779E-38 c Pressure 0.47946E-18 0 0.10000E+01 -0.47946E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010617 0.90208 0.14627 0.14627 v Velocity[Y] -4.5082e-18 1.493e-17 2.9892e-19 2.9892e-19 v Velocity[Z] -4.418e-18 5.898e-18 3.0242e-22 3.0242e-22 v ǁVelocityǁ 0.010617 0.90208 0.14627 0.14627 v Pressure 0 0 0 0 v CourantNb 0 3.331e-16 2.0695e-17 2.0695e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.283000000E+02 TIME STEP NUMBER 283 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26748E-11 0.98955E-01 Friction velocity uk : 0.26748E-11 0.98955E-01 Dimensionless distance yplus : 0.13374E-08 0.98955E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44303E-02 1460 0.89756E-08 0.53562E-05 0.10643E+00 c Velocity[X] 0.53562E-05 c Velocity[Y] 0.18768E-38 c Velocity[Z] 0.19513E-38 c Pressure 0.47992E-18 0 0.10000E+01 -0.47992E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010598 0.90225 0.14635 0.14635 v Velocity[Y] -4.5285e-18 1.4912e-17 2.9775e-19 2.9775e-19 v Velocity[Z] -4.4233e-18 5.9121e-18 -3.453e-23 -3.453e-23 v ǁVelocityǁ 0.010598 0.90225 0.14635 0.14635 v Pressure 0 0 0 0 v CourantNb 0 3.3281e-16 2.0715e-17 2.0715e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.284000000E+02 TIME STEP NUMBER 284 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27321E-11 0.98867E-01 Friction velocity uk : 0.27321E-11 0.98867E-01 Dimensionless distance yplus : 0.13660E-08 0.98867E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44333E-02 1459 0.90177E-08 0.53270E-05 0.10607E+00 c Velocity[X] 0.53270E-05 c Velocity[Y] 0.15932E-38 c Velocity[Z] 0.23501E-38 c Pressure 0.48042E-18 0 0.10000E+01 -0.48042E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010578 0.90242 0.14643 0.14643 v Velocity[Y] -4.5483e-18 1.4897e-17 2.9658e-19 2.9658e-19 v Velocity[Z] -4.4266e-18 5.8938e-18 -2.5077e-22 -2.5077e-22 v ǁVelocityǁ 0.010578 0.90242 0.14643 0.14643 v Pressure 0 0 0 0 v CourantNb 0 3.3314e-16 2.0728e-17 2.0728e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.285000000E+02 TIME STEP NUMBER 285 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21618E-11 0.98781E-01 Friction velocity uk : 0.21618E-11 0.98781E-01 Dimensionless distance yplus : 0.10809E-08 0.98781E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44364E-02 1459 0.89880E-08 0.52981E-05 0.10571E+00 c Velocity[X] 0.52981E-05 c Velocity[Y] 0.17255E-38 c Velocity[Z] 0.21091E-38 c Pressure 0.48085E-18 0 0.10000E+01 -0.48085E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010559 0.90259 0.14651 0.14651 v Velocity[Y] -4.5675e-18 1.488e-17 2.954e-19 2.954e-19 v Velocity[Z] -4.4588e-18 5.8874e-18 -5.231e-22 -5.231e-22 v ǁVelocityǁ 0.010559 0.90259 0.14651 0.14651 v Pressure 0 0 0 0 v CourantNb 0 3.3348e-16 2.0762e-17 2.0762e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.286000000E+02 TIME STEP NUMBER 286 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27169E-11 0.98694E-01 Friction velocity uk : 0.27169E-11 0.98694E-01 Dimensionless distance yplus : 0.13585E-08 0.98694E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44394E-02 1458 0.90303E-08 0.52694E-05 0.10535E+00 c Velocity[X] 0.52694E-05 c Velocity[Y] 0.18870E-38 c Velocity[Z] 0.25610E-38 c Pressure 0.48134E-18 0 0.10000E+01 -0.48134E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010539 0.90276 0.14659 0.14659 v Velocity[Y] -4.5861e-18 1.4862e-17 2.9422e-19 2.9422e-19 v Velocity[Z] -4.4238e-18 5.8967e-18 -5.4779e-22 -5.4779e-22 v ǁVelocityǁ 0.010539 0.90276 0.14659 0.14659 v Pressure 0 0 0 0 v CourantNb 0 3.3524e-16 2.078e-17 2.078e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.287000000E+02 TIME STEP NUMBER 287 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27009E-11 0.98609E-01 Friction velocity uk : 0.27009E-11 0.98609E-01 Dimensionless distance yplus : 0.13504E-08 0.98609E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44424E-02 1458 0.90007E-08 0.52410E-05 0.10499E+00 c Velocity[X] 0.52410E-05 c Velocity[Y] 0.15428E-38 c Velocity[Z] 0.28736E-38 c Pressure 0.48174E-18 0 0.10000E+01 -0.48174E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01052 0.90293 0.14667 0.14667 v Velocity[Y] -4.6062e-18 1.4848e-17 2.9303e-19 2.9303e-19 v Velocity[Z] -4.4505e-18 5.9034e-18 -4.1596e-22 -4.1596e-22 v ǁVelocityǁ 0.01052 0.90293 0.14667 0.14667 v Pressure 0 0 0 0 v CourantNb 0 3.3273e-16 2.08e-17 2.08e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.288000000E+02 TIME STEP NUMBER 288 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19205E-11 0.98523E-01 Friction velocity uk : 0.19205E-11 0.98523E-01 Dimensionless distance yplus : 0.96027E-09 0.98523E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44454E-02 1458 0.89713E-08 0.52128E-05 0.10463E+00 c Velocity[X] 0.52128E-05 c Velocity[Y] 0.16303E-38 c Velocity[Z] 0.22664E-38 c Pressure 0.48225E-18 0 0.10000E+01 -0.48225E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010501 0.9031 0.14675 0.14675 v Velocity[Y] -4.6261e-18 1.4834e-17 2.9185e-19 2.9185e-19 v Velocity[Z] -4.4703e-18 5.902e-18 -7.9234e-22 -7.9234e-22 v ǁVelocityǁ 0.010501 0.9031 0.14675 0.14675 v Pressure 0 0 0 0 v CourantNb 0 3.3409e-16 2.082e-17 2.082e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.289000000E+02 TIME STEP NUMBER 289 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25799E-11 0.98438E-01 Friction velocity uk : 0.25799E-11 0.98438E-01 Dimensionless distance yplus : 0.12900E-08 0.98438E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44484E-02 1457 0.90139E-08 0.51849E-05 0.10428E+00 c Velocity[X] 0.51849E-05 c Velocity[Y] 0.16523E-38 c Velocity[Z] 0.24102E-38 c Pressure 0.48277E-18 0 0.10000E+01 -0.48277E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010482 0.90327 0.14683 0.14683 v Velocity[Y] -4.6446e-18 1.4817e-17 2.9066e-19 2.9066e-19 v Velocity[Z] -4.4703e-18 5.9064e-18 -8.7978e-22 -8.7978e-22 v ǁVelocityǁ 0.010482 0.90327 0.14683 0.14683 v Pressure 0 0 0 0 v CourantNb 0 3.3539e-16 2.0834e-17 2.0834e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.290000000E+02 TIME STEP NUMBER 290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23514E-11 0.98353E-01 Friction velocity uk : 0.23514E-11 0.98353E-01 Dimensionless distance yplus : 0.11757E-08 0.98353E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44514E-02 1457 0.89846E-08 0.51573E-05 0.10393E+00 c Velocity[X] 0.51573E-05 c Velocity[Y] 0.17034E-38 c Velocity[Z] 0.22597E-38 c Pressure 0.48307E-18 0 0.10000E+01 -0.48307E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010463 0.90343 0.14691 0.14691 v Velocity[Y] -4.6652e-18 1.4801e-17 2.8946e-19 2.8946e-19 v Velocity[Z] -4.4531e-18 5.8985e-18 -1.0908e-21 -1.0908e-21 v ǁVelocityǁ 0.010463 0.90343 0.14691 0.14691 v Pressure 0 0 0 0 v CourantNb 0 3.3509e-16 2.0845e-17 2.0845e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.291000000E+02 TIME STEP NUMBER 291 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26612E-11 0.98269E-01 Friction velocity uk : 0.26612E-11 0.98269E-01 Dimensionless distance yplus : 0.13306E-08 0.98269E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44544E-02 1456 0.90274E-08 0.51298E-05 0.10358E+00 c Velocity[X] 0.51298E-05 c Velocity[Y] 0.18359E-38 c Velocity[Z] 0.28030E-38 c Pressure 0.48357E-18 0 0.10000E+01 -0.48357E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010444 0.9036 0.14699 0.14699 v Velocity[Y] -4.6853e-18 1.4786e-17 2.8827e-19 2.8827e-19 v Velocity[Z] -4.4583e-18 5.8958e-18 -8.5905e-22 -8.5905e-22 v ǁVelocityǁ 0.010444 0.9036 0.14699 0.14699 v Pressure 0 0 0 0 v CourantNb 0 3.3457e-16 2.0857e-17 2.0857e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.292000000E+02 TIME STEP NUMBER 292 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14050E-11 0.98185E-01 Friction velocity uk : 0.14050E-11 0.98185E-01 Dimensionless distance yplus : 0.70248E-09 0.98185E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44574E-02 1456 0.89983E-08 0.51026E-05 0.10323E+00 c Velocity[X] 0.51026E-05 c Velocity[Y] 0.19366E-38 c Velocity[Z] 0.23710E-38 c Pressure 0.48407E-18 0 0.10000E+01 -0.48407E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010426 0.90376 0.14707 0.14707 v Velocity[Y] -4.7042e-18 1.4768e-17 2.8706e-19 2.8706e-19 v Velocity[Z] -4.4832e-18 5.9041e-18 -3.5671e-22 -3.5671e-22 v ǁVelocityǁ 0.010426 0.90376 0.14707 0.14707 v Pressure 0 0 0 0 v CourantNb 0 3.3543e-16 2.0882e-17 2.0882e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.293000000E+02 TIME STEP NUMBER 293 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19756E-11 0.98101E-01 Friction velocity uk : 0.19756E-11 0.98101E-01 Dimensionless distance yplus : 0.98781E-09 0.98101E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44604E-02 1456 0.89693E-08 0.50757E-05 0.10289E+00 c Velocity[X] 0.50757E-05 c Velocity[Y] 0.17888E-38 c Velocity[Z] 0.26409E-38 c Pressure 0.48451E-18 0 0.10000E+01 -0.48451E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010407 0.90392 0.14715 0.14715 v Velocity[Y] -4.7241e-18 1.475e-17 2.8585e-19 2.8585e-19 v Velocity[Z] -4.4612e-18 5.916e-18 -6.7699e-22 -6.7699e-22 v ǁVelocityǁ 0.010407 0.90392 0.14715 0.14715 v Pressure 0 0 0 0 v CourantNb 0 3.3626e-16 2.0898e-17 2.0898e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.294000000E+02 TIME STEP NUMBER 294 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26239E-11 0.98018E-01 Friction velocity uk : 0.26239E-11 0.98018E-01 Dimensionless distance yplus : 0.13120E-08 0.98018E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44634E-02 1455 0.90124E-08 0.50490E-05 0.10255E+00 c Velocity[X] 0.50490E-05 c Velocity[Y] 0.18424E-38 c Velocity[Z] 0.15142E-38 c Pressure 0.48491E-18 0 0.10000E+01 -0.48491E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010389 0.90409 0.14723 0.14723 v Velocity[Y] -4.7439e-18 1.4729e-17 2.8464e-19 2.8464e-19 v Velocity[Z] -4.4627e-18 5.9102e-18 -7.6019e-22 -7.6019e-22 v ǁVelocityǁ 0.010389 0.90409 0.14723 0.14723 v Pressure 0 0 0 0 v CourantNb 0 3.3625e-16 2.0923e-17 2.0923e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.295000000E+02 TIME STEP NUMBER 295 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20875E-11 0.97935E-01 Friction velocity uk : 0.20875E-11 0.97935E-01 Dimensionless distance yplus : 0.10437E-08 0.97935E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44663E-02 1455 0.89835E-08 0.50225E-05 0.10221E+00 c Velocity[X] 0.50225E-05 c Velocity[Y] 0.17715E-38 c Velocity[Z] 0.19557E-38 c Pressure 0.48533E-18 0 0.10000E+01 -0.48533E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01037 0.90425 0.14731 0.14731 v Velocity[Y] -4.7633e-18 1.4712e-17 2.8343e-19 2.8343e-19 v Velocity[Z] -4.4594e-18 5.8985e-18 -9.4829e-22 -9.4829e-22 v ǁVelocityǁ 0.01037 0.90425 0.14731 0.14731 v Pressure 0 0 0 0 v CourantNb 0 3.3585e-16 2.0923e-17 2.0923e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.296000000E+02 TIME STEP NUMBER 296 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26135E-11 0.97853E-01 Friction velocity uk : 0.26135E-11 0.97853E-01 Dimensionless distance yplus : 0.13068E-08 0.97853E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44693E-02 1454 0.90269E-08 0.49962E-05 0.10187E+00 c Velocity[X] 0.49962E-05 c Velocity[Y] 0.17828E-38 c Velocity[Z] 0.16715E-38 c Pressure 0.48591E-18 0 0.10000E+01 -0.48591E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010352 0.90441 0.14739 0.14739 v Velocity[Y] -4.7826e-18 1.4692e-17 2.8221e-19 2.8221e-19 v Velocity[Z] -4.4793e-18 5.9099e-18 -7.8316e-22 -7.8316e-22 v ǁVelocityǁ 0.010352 0.90441 0.14739 0.14739 v Pressure 0 0 0 0 v CourantNb 0 3.3529e-16 2.094e-17 2.094e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.297000000E+02 TIME STEP NUMBER 297 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24187E-11 0.97771E-01 Friction velocity uk : 0.24187E-11 0.97771E-01 Dimensionless distance yplus : 0.12094E-08 0.97771E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44722E-02 1454 0.89982E-08 0.49702E-05 0.10154E+00 c Velocity[X] 0.49702E-05 c Velocity[Y] 0.17936E-38 c Velocity[Z] 0.16836E-38 c Pressure 0.48623E-18 0 0.10000E+01 -0.48623E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010334 0.90457 0.14747 0.14747 v Velocity[Y] -4.8017e-18 1.4675e-17 2.8099e-19 2.8099e-19 v Velocity[Z] -4.4706e-18 5.9257e-18 -2.2774e-22 -2.2774e-22 v ǁVelocityǁ 0.010334 0.90457 0.14747 0.14747 v Pressure 0 0 0 0 v CourantNb 0 3.3676e-16 2.0947e-17 2.0947e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.298000000E+02 TIME STEP NUMBER 298 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24636E-11 0.97689E-01 Friction velocity uk : 0.24636E-11 0.97689E-01 Dimensionless distance yplus : 0.12318E-08 0.97689E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44752E-02 1454 0.89697E-08 0.49444E-05 0.10120E+00 c Velocity[X] 0.49444E-05 c Velocity[Y] 0.17844E-38 c Velocity[Z] 0.13233E-38 c Pressure 0.48676E-18 0 0.10000E+01 -0.48676E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010316 0.90473 0.14755 0.14755 v Velocity[Y] -4.8211e-18 1.4658e-17 2.7977e-19 2.7977e-19 v Velocity[Z] -4.4725e-18 5.9147e-18 -4.3377e-22 -4.3377e-22 v ǁVelocityǁ 0.010316 0.90473 0.14755 0.14755 v Pressure 0 0 0 0 v CourantNb 0 3.3621e-16 2.0974e-17 2.0974e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.299000000E+02 TIME STEP NUMBER 299 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25487E-11 0.97607E-01 Friction velocity uk : 0.25487E-11 0.97607E-01 Dimensionless distance yplus : 0.12744E-08 0.97607E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44781E-02 1453 0.90132E-08 0.49188E-05 0.10087E+00 c Velocity[X] 0.49188E-05 c Velocity[Y] 0.17898E-38 c Velocity[Z] 0.15608E-38 c Pressure 0.48711E-18 0 0.10000E+01 -0.48711E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010298 0.90489 0.14763 0.14763 v Velocity[Y] -4.8397e-18 1.4638e-17 2.7854e-19 2.7854e-19 v Velocity[Z] -4.4553e-18 5.9245e-18 -2.4193e-22 -2.4193e-22 v ǁVelocityǁ 0.010298 0.90489 0.14763 0.14763 v Pressure 0 0 0 0 v CourantNb 0 3.3634e-16 2.0988e-17 2.0988e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.300000000E+02 TIME STEP NUMBER 300 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24991E-11 0.97526E-01 Friction velocity uk : 0.24991E-11 0.97526E-01 Dimensionless distance yplus : 0.12495E-08 0.97526E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 300, Physical time 0.30000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44810E-02 1453 0.89848E-08 0.48934E-05 0.10054E+00 c Velocity[X] 0.48934E-05 c Velocity[Y] 0.18911E-38 c Velocity[Z] 0.15634E-38 c Pressure 0.48752E-18 0 0.10000E+01 -0.48752E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.01028 0.90504 0.14771 0.14771 v Velocity[Y] -4.86e-18 1.4619e-17 2.7731e-19 2.7731e-19 v Velocity[Z] -4.4647e-18 5.9422e-18 -3.025e-22 -3.025e-22 v ǁVelocityǁ 0.01028 0.90504 0.14771 0.14771 v Pressure 0 0 0 0 v CourantNb 0 3.3563e-16 2.0998e-17 2.0998e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.301000000E+02 TIME STEP NUMBER 301 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25568E-11 0.97446E-01 Friction velocity uk : 0.25568E-11 0.97446E-01 Dimensionless distance yplus : 0.12784E-08 0.97446E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44840E-02 1452 0.90286E-08 0.48682E-05 0.10022E+00 c Velocity[X] 0.48682E-05 c Velocity[Y] 0.18245E-38 c Velocity[Z] 0.20549E-38 c Pressure 0.48799E-18 0 0.10000E+01 -0.48799E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010262 0.9052 0.14778 0.14778 v Velocity[Y] -4.8799e-18 1.4603e-17 2.7608e-19 2.7608e-19 v Velocity[Z] -4.469e-18 5.9277e-18 -6.8126e-22 -6.8126e-22 v ǁVelocityǁ 0.010262 0.9052 0.14778 0.14778 v Pressure 0 0 0 0 v CourantNb 0 3.3627e-16 2.1025e-17 2.1025e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.302000000E+02 TIME STEP NUMBER 302 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25317E-11 0.97365E-01 Friction velocity uk : 0.25317E-11 0.97365E-01 Dimensionless distance yplus : 0.12658E-08 0.97365E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44869E-02 1452 0.90004E-08 0.48433E-05 0.99895E-01 c Velocity[X] 0.48433E-05 c Velocity[Y] 0.16001E-38 c Velocity[Z] 0.24237E-38 c Pressure 0.48854E-18 0 0.10000E+01 -0.48854E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010244 0.90536 0.14786 0.14786 v Velocity[Y] -4.8984e-18 1.4587e-17 2.7484e-19 2.7484e-19 v Velocity[Z] -4.4805e-18 5.9355e-18 -5.5761e-22 -5.5761e-22 v ǁVelocityǁ 0.010244 0.90536 0.14786 0.14786 v Pressure 0 0 0 0 v CourantNb 0 3.3702e-16 2.1034e-17 2.1034e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.303000000E+02 TIME STEP NUMBER 303 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23241E-11 0.97285E-01 Friction velocity uk : 0.23241E-11 0.97285E-01 Dimensionless distance yplus : 0.11620E-08 0.97285E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44898E-02 1452 0.89723E-08 0.48185E-05 0.99573E-01 c Velocity[X] 0.48185E-05 c Velocity[Y] 0.17211E-38 c Velocity[Z] 0.20369E-38 c Pressure 0.48884E-18 0 0.10000E+01 -0.48884E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010226 0.90551 0.14794 0.14794 v Velocity[Y] -4.9179e-18 1.4571e-17 2.736e-19 2.736e-19 v Velocity[Z] -4.4607e-18 5.9221e-18 -6.918e-22 -6.918e-22 v ǁVelocityǁ 0.010226 0.90551 0.14794 0.14794 v Pressure 0 0 0 0 v CourantNb 0 3.3694e-16 2.1059e-17 2.1059e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.304000000E+02 TIME STEP NUMBER 304 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15582E-11 0.97206E-01 Friction velocity uk : 0.15582E-11 0.97206E-01 Dimensionless distance yplus : 0.77909E-09 0.97206E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44927E-02 1451 0.90163E-08 0.47940E-05 0.99253E-01 c Velocity[X] 0.47940E-05 c Velocity[Y] 0.17802E-38 c Velocity[Z] 0.19453E-38 c Pressure 0.48916E-18 0 0.10000E+01 -0.48916E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010209 0.90567 0.14802 0.14802 v Velocity[Y] -4.9362e-18 1.455e-17 2.7235e-19 2.7235e-19 v Velocity[Z] -4.4774e-18 5.9269e-18 -3.8532e-22 -3.8532e-22 v ǁVelocityǁ 0.010209 0.90567 0.14802 0.14802 v Pressure 0 0 0 0 v CourantNb 0 3.3663e-16 2.1068e-17 2.1068e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.305000000E+02 TIME STEP NUMBER 305 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25449E-11 0.97126E-01 Friction velocity uk : 0.25449E-11 0.97126E-01 Dimensionless distance yplus : 0.12724E-08 0.97126E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44956E-02 1451 0.89884E-08 0.47696E-05 0.98935E-01 c Velocity[X] 0.47696E-05 c Velocity[Y] 0.16594E-38 c Velocity[Z] 0.33767E-38 c Pressure 0.48976E-18 0 0.10000E+01 -0.48976E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010191 0.90582 0.1481 0.1481 v Velocity[Y] -4.956e-18 1.4537e-17 2.7111e-19 2.7111e-19 v Velocity[Z] -4.4437e-18 5.9439e-18 -3.1811e-22 -3.1811e-22 v ǁVelocityǁ 0.010191 0.90582 0.1481 0.1481 v Pressure 0 0 0 0 v CourantNb 0 3.3706e-16 2.1081e-17 2.1081e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.306000000E+02 TIME STEP NUMBER 306 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23739E-11 0.97047E-01 Friction velocity uk : 0.23739E-11 0.97047E-01 Dimensionless distance yplus : 0.11869E-08 0.97047E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44985E-02 1450 0.90326E-08 0.47455E-05 0.98619E-01 c Velocity[X] 0.47455E-05 c Velocity[Y] 0.16835E-38 c Velocity[Z] 0.18522E-38 c Pressure 0.49012E-18 0 0.10000E+01 -0.49012E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010174 0.90597 0.14818 0.14818 v Velocity[Y] -4.975e-18 1.452e-17 2.6986e-19 2.6986e-19 v Velocity[Z] -4.4638e-18 5.9372e-18 -3.7424e-22 -3.7424e-22 v ǁVelocityǁ 0.010174 0.90597 0.14818 0.14818 v Pressure 0 0 0 0 v CourantNb 0 3.3642e-16 2.1105e-17 2.1105e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.307000000E+02 TIME STEP NUMBER 307 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21825E-11 0.96969E-01 Friction velocity uk : 0.21825E-11 0.96969E-01 Dimensionless distance yplus : 0.10912E-08 0.96969E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45013E-02 1450 0.90048E-08 0.47216E-05 0.98305E-01 c Velocity[X] 0.47216E-05 c Velocity[Y] 0.14671E-38 c Velocity[Z] 0.22550E-38 c Pressure 0.49071E-18 0 0.10000E+01 -0.49071E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010156 0.90612 0.14825 0.14825 v Velocity[Y] -4.994e-18 1.4505e-17 2.6862e-19 2.6862e-19 v Velocity[Z] -4.4506e-18 5.953e-18 7.2948e-23 7.2948e-23 v ǁVelocityǁ 0.010156 0.90612 0.14825 0.14825 v Pressure 0 0 0 0 v CourantNb 0 3.3544e-16 2.1126e-17 2.1126e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.308000000E+02 TIME STEP NUMBER 308 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23975E-11 0.96890E-01 Friction velocity uk : 0.23975E-11 0.96890E-01 Dimensionless distance yplus : 0.11987E-08 0.96890E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45042E-02 1450 0.89772E-08 0.46978E-05 0.97994E-01 c Velocity[X] 0.46978E-05 c Velocity[Y] 0.15266E-38 c Velocity[Z] 0.28735E-38 c Pressure 0.49093E-18 0 0.10000E+01 -0.49093E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010139 0.90627 0.14833 0.14833 v Velocity[Y] -5.0139e-18 1.4493e-17 2.6737e-19 2.6737e-19 v Velocity[Z] -4.457e-18 5.9693e-18 3.3251e-22 3.3251e-22 v ǁVelocityǁ 0.010139 0.90627 0.14833 0.14833 v Pressure 0 0 0 0 v CourantNb 0 3.3747e-16 2.1146e-17 2.1146e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.309000000E+02 TIME STEP NUMBER 309 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19442E-11 0.96812E-01 Friction velocity uk : 0.19442E-11 0.96812E-01 Dimensionless distance yplus : 0.97208E-09 0.96812E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45071E-02 1449 0.90216E-08 0.46743E-05 0.97684E-01 c Velocity[X] 0.46743E-05 c Velocity[Y] 0.13811E-38 c Velocity[Z] 0.21833E-38 c Pressure 0.49155E-18 0 0.10000E+01 -0.49155E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010122 0.90642 0.14841 0.14841 v Velocity[Y] -5.0329e-18 1.4481e-17 2.6613e-19 2.6613e-19 v Velocity[Z] -4.4642e-18 5.9583e-18 -6.694e-23 -6.694e-23 v ǁVelocityǁ 0.010122 0.90642 0.14841 0.14841 v Pressure 0 0 0 0 v CourantNb 0 3.3654e-16 2.1168e-17 2.1168e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.310000000E+02 TIME STEP NUMBER 310 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24832E-11 0.96735E-01 Friction velocity uk : 0.24832E-11 0.96735E-01 Dimensionless distance yplus : 0.12416E-08 0.96735E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45099E-02 1449 0.89941E-08 0.46509E-05 0.97376E-01 c Velocity[X] 0.46509E-05 c Velocity[Y] 0.16590E-38 c Velocity[Z] 0.18158E-38 c Pressure 0.49197E-18 0 0.10000E+01 -0.49197E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010105 0.90657 0.14849 0.14849 v Velocity[Y] -5.0522e-18 1.4466e-17 2.6488e-19 2.6488e-19 v Velocity[Z] -4.465e-18 5.9599e-18 1.2874e-22 1.2874e-22 v ǁVelocityǁ 0.010105 0.90657 0.14849 0.14849 v Pressure 0 0 0 0 v CourantNb 0 3.3722e-16 2.1181e-17 2.1181e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.311000000E+02 TIME STEP NUMBER 311 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24641E-11 0.96657E-01 Friction velocity uk : 0.24641E-11 0.96657E-01 Dimensionless distance yplus : 0.12321E-08 0.96657E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45128E-02 1448 0.90388E-08 0.46278E-05 0.97070E-01 c Velocity[X] 0.46278E-05 c Velocity[Y] 0.15937E-38 c Velocity[Z] 0.31185E-38 c Pressure 0.49232E-18 0 0.10000E+01 -0.49232E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010088 0.90672 0.14856 0.14856 v Velocity[Y] -5.0709e-18 1.4449e-17 2.6363e-19 2.6363e-19 v Velocity[Z] -4.4731e-18 5.9579e-18 -5.4104e-22 -5.4104e-22 v ǁVelocityǁ 0.010088 0.90672 0.14856 0.14856 v Pressure 0 0 0 0 v CourantNb 0 3.3696e-16 2.1205e-17 2.1205e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.312000000E+02 TIME STEP NUMBER 312 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24541E-11 0.96580E-01 Friction velocity uk : 0.24541E-11 0.96580E-01 Dimensionless distance yplus : 0.12270E-08 0.96580E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45156E-02 1448 0.90114E-08 0.46048E-05 0.96766E-01 c Velocity[X] 0.46048E-05 c Velocity[Y] 0.17528E-38 c Velocity[Z] 0.22680E-38 c Pressure 0.49272E-18 0 0.10000E+01 -0.49272E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010071 0.90687 0.14864 0.14864 v Velocity[Y] -5.0896e-18 1.4434e-17 2.6238e-19 2.6238e-19 v Velocity[Z] -4.4714e-18 5.9423e-18 -2.218e-22 -2.218e-22 v ǁVelocityǁ 0.010071 0.90687 0.14864 0.14864 v Pressure 0 0 0 0 v CourantNb 0 3.378e-16 2.1203e-17 2.1203e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.313000000E+02 TIME STEP NUMBER 313 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24194E-11 0.96503E-01 Friction velocity uk : 0.24194E-11 0.96503E-01 Dimensionless distance yplus : 0.12097E-08 0.96503E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45185E-02 1448 0.89841E-08 0.45820E-05 0.96464E-01 c Velocity[X] 0.45820E-05 c Velocity[Y] 0.16096E-38 c Velocity[Z] 0.16330E-38 c Pressure 0.49313E-18 0 0.10000E+01 -0.49313E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010054 0.90702 0.14872 0.14872 v Velocity[Y] -5.1101e-18 1.4418e-17 2.6113e-19 2.6113e-19 v Velocity[Z] -4.4612e-18 5.9644e-18 -2.7126e-22 -2.7126e-22 v ǁVelocityǁ 0.010054 0.90702 0.14872 0.14872 v Pressure 0 0 0 0 v CourantNb 0 3.3824e-16 2.123e-17 2.123e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.314000000E+02 TIME STEP NUMBER 314 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23981E-11 0.96427E-01 Friction velocity uk : 0.23981E-11 0.96427E-01 Dimensionless distance yplus : 0.11991E-08 0.96427E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45213E-02 1447 0.90290E-08 0.45594E-05 0.96164E-01 c Velocity[X] 0.45594E-05 c Velocity[Y] 0.15267E-38 c Velocity[Z] 0.22904E-38 c Pressure 0.49341E-18 0 0.10000E+01 -0.49341E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010038 0.90716 0.14879 0.14879 v Velocity[Y] -5.1277e-18 1.4403e-17 2.5988e-19 2.5988e-19 v Velocity[Z] -4.4498e-18 5.9673e-18 -2.6416e-24 -2.6416e-24 v ǁVelocityǁ 0.010038 0.90716 0.14879 0.14879 v Pressure 0 0 0 0 v CourantNb 0 3.3769e-16 2.1244e-17 2.1244e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.315000000E+02 TIME STEP NUMBER 315 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17417E-11 0.96351E-01 Friction velocity uk : 0.17417E-11 0.96351E-01 Dimensionless distance yplus : 0.87087E-09 0.96351E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45241E-02 1447 0.90019E-08 0.45370E-05 0.95865E-01 c Velocity[X] 0.45370E-05 c Velocity[Y] 0.17423E-38 c Velocity[Z] 0.18247E-38 c Pressure 0.49398E-18 0 0.10000E+01 -0.49398E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010021 0.90731 0.14887 0.14887 v Velocity[Y] -5.1466e-18 1.4384e-17 2.5862e-19 2.5862e-19 v Velocity[Z] -4.4486e-18 5.952e-18 1.191e-23 1.191e-23 v ǁVelocityǁ 0.010021 0.90731 0.14887 0.14887 v Pressure 0 0 0 0 v CourantNb 0 3.3681e-16 2.1256e-17 2.1256e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.316000000E+02 TIME STEP NUMBER 316 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23244E-11 0.96275E-01 Friction velocity uk : 0.23244E-11 0.96275E-01 Dimensionless distance yplus : 0.11622E-08 0.96275E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45269E-02 1447 0.89749E-08 0.45147E-05 0.95569E-01 c Velocity[X] 0.45147E-05 c Velocity[Y] 0.15600E-38 c Velocity[Z] 0.22507E-38 c Pressure 0.49447E-18 0 0.10000E+01 -0.49447E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010004 0.90746 0.14895 0.14895 v Velocity[Y] -5.1653e-18 1.437e-17 2.5736e-19 2.5736e-19 v Velocity[Z] -4.4609e-18 5.947e-18 -2.9325e-22 -2.9325e-22 v ǁVelocityǁ 0.010004 0.90746 0.14895 0.14895 v Pressure 0 0 0 0 v CourantNb 0 3.3744e-16 2.1254e-17 2.1254e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.317000000E+02 TIME STEP NUMBER 317 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23154E-11 0.96200E-01 Friction velocity uk : 0.23154E-11 0.96200E-01 Dimensionless distance yplus : 0.11577E-08 0.96200E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45297E-02 1446 0.90200E-08 0.44927E-05 0.95274E-01 c Velocity[X] 0.44927E-05 c Velocity[Y] 0.16574E-38 c Velocity[Z] 0.16463E-38 c Pressure 0.49475E-18 0 0.10000E+01 -0.49475E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0099878 0.9076 0.14902 0.14902 v Velocity[Y] -5.1838e-18 1.4353e-17 2.5609e-19 2.5609e-19 v Velocity[Z] -4.475e-18 5.9429e-18 -2.6957e-24 -2.6957e-24 v ǁVelocityǁ 0.0099878 0.9076 0.14902 0.14902 v Pressure 0 0 0 0 v CourantNb 0 3.3797e-16 2.129e-17 2.129e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.318000000E+02 TIME STEP NUMBER 318 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23169E-11 0.96125E-01 Friction velocity uk : 0.23169E-11 0.96125E-01 Dimensionless distance yplus : 0.11585E-08 0.96125E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45325E-02 1446 0.89931E-08 0.44708E-05 0.94981E-01 c Velocity[X] 0.44708E-05 c Velocity[Y] 0.15970E-38 c Velocity[Z] 0.18671E-38 c Pressure 0.49524E-18 0 0.10000E+01 -0.49524E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0099714 0.90774 0.1491 0.1491 v Velocity[Y] -5.2024e-18 1.4339e-17 2.5483e-19 2.5483e-19 v Velocity[Z] -4.4353e-18 5.9604e-18 -2.5662e-22 -2.5662e-22 v ǁVelocityǁ 0.0099714 0.90774 0.1491 0.1491 v Pressure 0 0 0 0 v CourantNb 0 3.3785e-16 2.1284e-17 2.1284e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.319000000E+02 TIME STEP NUMBER 319 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22971E-11 0.96050E-01 Friction velocity uk : 0.22971E-11 0.96050E-01 Dimensionless distance yplus : 0.11486E-08 0.96050E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45353E-02 1445 0.90385E-08 0.44491E-05 0.94690E-01 c Velocity[X] 0.44491E-05 c Velocity[Y] 0.16294E-38 c Velocity[Z] 0.20926E-38 c Pressure 0.49549E-18 0 0.10000E+01 -0.49549E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0099551 0.90789 0.14918 0.14918 v Velocity[Y] -5.2214e-18 1.4322e-17 2.5356e-19 2.5356e-19 v Velocity[Z] -4.4598e-18 5.9466e-18 -9.3864e-23 -9.3864e-23 v ǁVelocityǁ 0.0099551 0.90789 0.14918 0.14918 v Pressure 0 0 0 0 v CourantNb 0 3.3709e-16 2.1315e-17 2.1315e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.320000000E+02 TIME STEP NUMBER 320 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23008E-11 0.95975E-01 Friction velocity uk : 0.23008E-11 0.95975E-01 Dimensionless distance yplus : 0.11504E-08 0.95975E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45381E-02 1445 0.90117E-08 0.44275E-05 0.94401E-01 c Velocity[X] 0.44275E-05 c Velocity[Y] 0.16597E-38 c Velocity[Z] 0.17447E-38 c Pressure 0.49607E-18 0 0.10000E+01 -0.49607E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0099388 0.90803 0.14925 0.14925 v Velocity[Y] -5.2404e-18 1.4306e-17 2.5229e-19 2.5229e-19 v Velocity[Z] -4.4808e-18 5.9646e-18 5.8864e-23 5.8864e-23 v ǁVelocityǁ 0.0099388 0.90803 0.14925 0.14925 v Pressure 0 0 0 0 v CourantNb 0 3.3818e-16 2.1307e-17 2.1307e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.321000000E+02 TIME STEP NUMBER 321 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22683E-11 0.95901E-01 Friction velocity uk : 0.22683E-11 0.95901E-01 Dimensionless distance yplus : 0.11341E-08 0.95901E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45409E-02 1445 0.89851E-08 0.44062E-05 0.94113E-01 c Velocity[X] 0.44062E-05 c Velocity[Y] 0.17286E-38 c Velocity[Z] 0.21843E-38 c Pressure 0.49648E-18 0 0.10000E+01 -0.49648E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0099226 0.90817 0.14933 0.14933 v Velocity[Y] -5.2609e-18 1.4293e-17 2.5102e-19 2.5102e-19 v Velocity[Z] -4.4724e-18 5.9744e-18 -6.0314e-22 -6.0314e-22 v ǁVelocityǁ 0.0099226 0.90817 0.14933 0.14933 v Pressure 0 0 0 0 v CourantNb 0 3.387e-16 2.1328e-17 2.1328e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.322000000E+02 TIME STEP NUMBER 322 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22690E-11 0.95827E-01 Friction velocity uk : 0.22690E-11 0.95827E-01 Dimensionless distance yplus : 0.11345E-08 0.95827E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45437E-02 1444 0.90306E-08 0.43850E-05 0.93828E-01 c Velocity[X] 0.43850E-05 c Velocity[Y] 0.16294E-38 c Velocity[Z] 0.21017E-38 c Pressure 0.49680E-18 0 0.10000E+01 -0.49680E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0099065 0.90831 0.1494 0.1494 v Velocity[Y] -5.2791e-18 1.4277e-17 2.4975e-19 2.4975e-19 v Velocity[Z] -4.47e-18 5.9411e-18 -3.0075e-22 -3.0075e-22 v ǁVelocityǁ 0.0099065 0.90831 0.1494 0.1494 v Pressure 0 0 0 0 v CourantNb 0 3.3854e-16 2.1359e-17 2.1359e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.323000000E+02 TIME STEP NUMBER 323 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21897E-11 0.95754E-01 Friction velocity uk : 0.21897E-11 0.95754E-01 Dimensionless distance yplus : 0.10948E-08 0.95754E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45464E-02 1444 0.90041E-08 0.43639E-05 0.93544E-01 c Velocity[X] 0.43639E-05 c Velocity[Y] 0.16702E-38 c Velocity[Z] 0.15704E-38 c Pressure 0.49733E-18 0 0.10000E+01 -0.49733E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0098905 0.90845 0.14948 0.14948 v Velocity[Y] -5.2988e-18 1.4262e-17 2.4847e-19 2.4847e-19 v Velocity[Z] -4.4901e-18 5.9812e-18 -1.634e-22 -1.634e-22 v ǁVelocityǁ 0.0098905 0.90845 0.14948 0.14948 v Pressure 0 0 0 0 v CourantNb 0 3.3906e-16 2.1369e-17 2.1369e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.324000000E+02 TIME STEP NUMBER 324 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22888E-11 0.95680E-01 Friction velocity uk : 0.22888E-11 0.95680E-01 Dimensionless distance yplus : 0.11444E-08 0.95680E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45492E-02 1444 0.89778E-08 0.43431E-05 0.93261E-01 c Velocity[X] 0.43431E-05 c Velocity[Y] 0.18325E-38 c Velocity[Z] 0.25505E-38 c Pressure 0.49767E-18 0 0.10000E+01 -0.49767E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0098745 0.90859 0.14955 0.14955 v Velocity[Y] -5.3189e-18 1.4243e-17 2.4719e-19 2.4719e-19 v Velocity[Z] -4.4457e-18 5.9535e-18 -1.9284e-22 -1.9284e-22 v ǁVelocityǁ 0.0098745 0.90859 0.14955 0.14955 v Pressure 0 0 0 0 v CourantNb 0 3.3923e-16 2.1386e-17 2.1386e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.325000000E+02 TIME STEP NUMBER 325 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21497E-11 0.95607E-01 Friction velocity uk : 0.21497E-11 0.95607E-01 Dimensionless distance yplus : 0.10748E-08 0.95607E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45520E-02 1443 0.90235E-08 0.43224E-05 0.92981E-01 c Velocity[X] 0.43224E-05 c Velocity[Y] 0.16919E-38 c Velocity[Z] 0.21432E-38 c Pressure 0.49799E-18 0 0.10000E+01 -0.49799E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0098586 0.90873 0.14963 0.14963 v Velocity[Y] -5.3386e-18 1.4228e-17 2.4591e-19 2.4591e-19 v Velocity[Z] -4.4843e-18 5.9507e-18 -3.3387e-22 -3.3387e-22 v ǁVelocityǁ 0.0098586 0.90873 0.14963 0.14963 v Pressure 0 0 0 0 v CourantNb 0 3.3832e-16 2.1388e-17 2.1388e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.326000000E+02 TIME STEP NUMBER 326 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22634E-11 0.95535E-01 Friction velocity uk : 0.22634E-11 0.95535E-01 Dimensionless distance yplus : 0.11317E-08 0.95535E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45547E-02 1443 0.89973E-08 0.43018E-05 0.92702E-01 c Velocity[X] 0.43018E-05 c Velocity[Y] 0.17777E-38 c Velocity[Z] 0.28913E-38 c Pressure 0.49854E-18 0 0.10000E+01 -0.49854E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0098428 0.90887 0.14971 0.14971 v Velocity[Y] -5.3589e-18 1.4212e-17 2.4462e-19 2.4462e-19 v Velocity[Z] -4.4832e-18 6.0006e-18 -3.1291e-22 -3.1291e-22 v ǁVelocityǁ 0.0098428 0.90887 0.14971 0.14971 v Pressure 0 0 0 0 v CourantNb 0 3.3999e-16 2.1407e-17 2.1407e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.327000000E+02 TIME STEP NUMBER 327 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22327E-11 0.95462E-01 Friction velocity uk : 0.22327E-11 0.95462E-01 Dimensionless distance yplus : 0.11163E-08 0.95462E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45575E-02 1443 0.89712E-08 0.42814E-05 0.92424E-01 c Velocity[X] 0.42814E-05 c Velocity[Y] 0.15944E-38 c Velocity[Z] 0.22679E-38 c Pressure 0.49905E-18 0 0.10000E+01 -0.49905E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0098271 0.90901 0.14978 0.14978 v Velocity[Y] -5.3773e-18 1.4198e-17 2.4333e-19 2.4333e-19 v Velocity[Z] -4.4949e-18 5.9666e-18 -2.9528e-22 -2.9528e-22 v ǁVelocityǁ 0.0098271 0.90901 0.14978 0.14978 v Pressure 0 0 0 0 v CourantNb 0 3.3965e-16 2.1444e-17 2.1444e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.328000000E+02 TIME STEP NUMBER 328 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21816E-11 0.95390E-01 Friction velocity uk : 0.21816E-11 0.95390E-01 Dimensionless distance yplus : 0.10908E-08 0.95390E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45602E-02 1442 0.90171E-08 0.42612E-05 0.92149E-01 c Velocity[X] 0.42612E-05 c Velocity[Y] 0.17432E-38 c Velocity[Z] 0.21730E-38 c Pressure 0.49944E-18 0 0.10000E+01 -0.49944E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0098114 0.90914 0.14986 0.14986 v Velocity[Y] -5.3966e-18 1.4183e-17 2.4204e-19 2.4204e-19 v Velocity[Z] -4.5045e-18 5.9961e-18 -2.4026e-22 -2.4026e-22 v ǁVelocityǁ 0.0098114 0.90914 0.14986 0.14986 v Pressure 0 0 0 0 v CourantNb 0 3.4022e-16 2.1453e-17 2.1453e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.329000000E+02 TIME STEP NUMBER 329 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21986E-11 0.95318E-01 Friction velocity uk : 0.21986E-11 0.95318E-01 Dimensionless distance yplus : 0.10993E-08 0.95318E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45629E-02 1442 0.89911E-08 0.42411E-05 0.91875E-01 c Velocity[X] 0.42411E-05 c Velocity[Y] 0.17172E-38 c Velocity[Z] 0.17768E-38 c Pressure 0.49995E-18 0 0.10000E+01 -0.49995E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0097958 0.90928 0.14993 0.14993 v Velocity[Y] -5.416e-18 1.4167e-17 2.4075e-19 2.4075e-19 v Velocity[Z] -4.5056e-18 6.0004e-18 -2.1571e-22 -2.1571e-22 v ǁVelocityǁ 0.0097958 0.90928 0.14993 0.14993 v Pressure 0 0 0 0 v CourantNb 0 3.3981e-16 2.1479e-17 2.1479e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.330000000E+02 TIME STEP NUMBER 330 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22020E-11 0.95246E-01 Friction velocity uk : 0.22020E-11 0.95246E-01 Dimensionless distance yplus : 0.11010E-08 0.95246E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45657E-02 1441 0.90373E-08 0.42212E-05 0.91602E-01 c Velocity[X] 0.42212E-05 c Velocity[Y] 0.18451E-38 c Velocity[Z] 0.16651E-38 c Pressure 0.50035E-18 0 0.10000E+01 -0.50035E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0097803 0.90942 0.15001 0.15001 v Velocity[Y] -5.436e-18 1.415e-17 2.3945e-19 2.3945e-19 v Velocity[Z] -4.4984e-18 6.0005e-18 -3.2426e-22 -3.2426e-22 v ǁVelocityǁ 0.0097803 0.90942 0.15001 0.15001 v Pressure 0 0 0 0 v CourantNb 0 3.407e-16 2.1504e-17 2.1504e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.331000000E+02 TIME STEP NUMBER 331 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21483E-11 0.95175E-01 Friction velocity uk : 0.21483E-11 0.95175E-01 Dimensionless distance yplus : 0.10741E-08 0.95175E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45684E-02 1441 0.90114E-08 0.42014E-05 0.91332E-01 c Velocity[X] 0.42014E-05 c Velocity[Y] 0.17284E-38 c Velocity[Z] 0.23244E-38 c Pressure 0.50062E-18 0 0.10000E+01 -0.50062E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0097649 0.90955 0.15008 0.15008 v Velocity[Y] -5.4566e-18 1.4135e-17 2.3816e-19 2.3816e-19 v Velocity[Z] -4.4897e-18 5.9985e-18 8.4628e-23 8.4628e-23 v ǁVelocityǁ 0.0097649 0.90955 0.15008 0.15008 v Pressure 0 0 0 0 v CourantNb 0 3.4056e-16 2.1524e-17 2.1524e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.332000000E+02 TIME STEP NUMBER 332 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21867E-11 0.95104E-01 Friction velocity uk : 0.21867E-11 0.95104E-01 Dimensionless distance yplus : 0.10933E-08 0.95104E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45711E-02 1441 0.89856E-08 0.41818E-05 0.91063E-01 c Velocity[X] 0.41818E-05 c Velocity[Y] 0.16767E-38 c Velocity[Z] 0.13793E-38 c Pressure 0.50111E-18 0 0.10000E+01 -0.50111E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0097495 0.90969 0.15015 0.15015 v Velocity[Y] -5.4759e-18 1.4119e-17 2.3686e-19 2.3686e-19 v Velocity[Z] -4.4949e-18 6.0121e-18 -1.2627e-22 -1.2627e-22 v ǁVelocityǁ 0.0097495 0.90969 0.15015 0.15015 v Pressure 0 0 0 0 v CourantNb 0 3.4031e-16 2.1528e-17 2.1528e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.333000000E+02 TIME STEP NUMBER 333 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17622E-11 0.95033E-01 Friction velocity uk : 0.17622E-11 0.95033E-01 Dimensionless distance yplus : 0.88112E-09 0.95033E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45738E-02 1440 0.90320E-08 0.41623E-05 0.90795E-01 c Velocity[X] 0.41623E-05 c Velocity[Y] 0.16543E-38 c Velocity[Z] 0.20850E-38 c Pressure 0.50158E-18 0 0.10000E+01 -0.50158E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0097342 0.90982 0.15023 0.15023 v Velocity[Y] -5.4953e-18 1.4106e-17 2.3556e-19 2.3556e-19 v Velocity[Z] -4.4775e-18 5.9992e-18 -4.9192e-23 -4.9192e-23 v ǁVelocityǁ 0.0097342 0.90982 0.15023 0.15023 v Pressure 0 0 0 0 v CourantNb 0 3.4128e-16 2.1537e-17 2.1537e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.334000000E+02 TIME STEP NUMBER 334 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20420E-11 0.94963E-01 Friction velocity uk : 0.20420E-11 0.94963E-01 Dimensionless distance yplus : 0.10210E-08 0.94963E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45765E-02 1440 0.90063E-08 0.41430E-05 0.90529E-01 c Velocity[X] 0.41430E-05 c Velocity[Y] 0.16118E-38 c Velocity[Z] 0.23368E-38 c Pressure 0.50186E-18 0 0.10000E+01 -0.50186E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0097189 0.90995 0.1503 0.1503 v Velocity[Y] -5.5156e-18 1.4094e-17 2.3426e-19 2.3426e-19 v Velocity[Z] -4.4988e-18 6.0081e-18 -1.3695e-22 -1.3695e-22 v ǁVelocityǁ 0.0097189 0.90995 0.1503 0.1503 v Pressure 0 0 0 0 v CourantNb 0 3.403e-16 2.1555e-17 2.1555e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.335000000E+02 TIME STEP NUMBER 335 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16075E-11 0.94893E-01 Friction velocity uk : 0.16075E-11 0.94893E-01 Dimensionless distance yplus : 0.80375E-09 0.94893E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45792E-02 1440 0.89808E-08 0.41239E-05 0.90265E-01 c Velocity[X] 0.41239E-05 c Velocity[Y] 0.17464E-38 c Velocity[Z] 0.22016E-38 c Pressure 0.50231E-18 0 0.10000E+01 -0.50231E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0097038 0.91009 0.15038 0.15038 v Velocity[Y] -5.5354e-18 1.4079e-17 2.3295e-19 2.3295e-19 v Velocity[Z] -4.4749e-18 5.9979e-18 -4.5178e-22 -4.5178e-22 v ǁVelocityǁ 0.0097038 0.91009 0.15038 0.15038 v Pressure 0 0 0 0 v CourantNb 0 3.4051e-16 2.1578e-17 2.1578e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.336000000E+02 TIME STEP NUMBER 336 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21410E-11 0.94823E-01 Friction velocity uk : 0.21410E-11 0.94823E-01 Dimensionless distance yplus : 0.10705E-08 0.94823E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45819E-02 1439 0.90274E-08 0.41048E-05 0.90002E-01 c Velocity[X] 0.41048E-05 c Velocity[Y] 0.15889E-38 c Velocity[Z] 0.30253E-38 c Pressure 0.50274E-18 0 0.10000E+01 -0.50274E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0096887 0.91022 0.15045 0.15045 v Velocity[Y] -5.5538e-18 1.4063e-17 2.3165e-19 2.3165e-19 v Velocity[Z] -4.5036e-18 5.996e-18 -4.0586e-22 -4.0586e-22 v ǁVelocityǁ 0.0096887 0.91022 0.15045 0.15045 v Pressure 0 0 0 0 v CourantNb 0 3.4026e-16 2.1578e-17 2.1578e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.337000000E+02 TIME STEP NUMBER 337 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19452E-11 0.94753E-01 Friction velocity uk : 0.19452E-11 0.94753E-01 Dimensionless distance yplus : 0.97260E-09 0.94753E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45846E-02 1439 0.90019E-08 0.40859E-05 0.89740E-01 c Velocity[X] 0.40859E-05 c Velocity[Y] 0.18381E-38 c Velocity[Z] 0.20489E-38 c Pressure 0.50321E-18 0 0.10000E+01 -0.50321E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0096736 0.91035 0.15053 0.15053 v Velocity[Y] -5.5744e-18 1.4047e-17 2.3034e-19 2.3034e-19 v Velocity[Z] -4.4804e-18 5.9969e-18 -2.6124e-22 -2.6124e-22 v ǁVelocityǁ 0.0096736 0.91035 0.15053 0.15053 v Pressure 0 0 0 0 v CourantNb 0 3.416e-16 2.1603e-17 2.1603e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.338000000E+02 TIME STEP NUMBER 338 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21349E-11 0.94684E-01 Friction velocity uk : 0.21349E-11 0.94684E-01 Dimensionless distance yplus : 0.10674E-08 0.94684E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45872E-02 1439 0.89766E-08 0.40672E-05 0.89480E-01 c Velocity[X] 0.40672E-05 c Velocity[Y] 0.17161E-38 c Velocity[Z] 0.21462E-38 c Pressure 0.50361E-18 0 0.10000E+01 -0.50361E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0096587 0.91048 0.1506 0.1506 v Velocity[Y] -5.5945e-18 1.4031e-17 2.2903e-19 2.2903e-19 v Velocity[Z] -4.5041e-18 5.996e-18 -8.1821e-22 -8.1821e-22 v ǁVelocityǁ 0.0096587 0.91048 0.1506 0.1506 v Pressure 0 0 0 0 v CourantNb 0 3.4127e-16 2.1615e-17 2.1615e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.339000000E+02 TIME STEP NUMBER 339 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21233E-11 0.94615E-01 Friction velocity uk : 0.21233E-11 0.94615E-01 Dimensionless distance yplus : 0.10617E-08 0.94615E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45899E-02 1438 0.90234E-08 0.40486E-05 0.89222E-01 c Velocity[X] 0.40486E-05 c Velocity[Y] 0.18295E-38 c Velocity[Z] 0.17061E-38 c Pressure 0.50402E-18 0 0.10000E+01 -0.50402E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0096438 0.91061 0.15067 0.15067 v Velocity[Y] -5.6145e-18 1.4015e-17 2.2771e-19 2.2771e-19 v Velocity[Z] -4.5078e-18 5.9903e-18 -8.2598e-22 -8.2598e-22 v ǁVelocityǁ 0.0096438 0.91061 0.15067 0.15067 v Pressure 0 0 0 0 v CourantNb 0 3.4202e-16 2.1639e-17 2.1639e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.340000000E+02 TIME STEP NUMBER 340 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21221E-11 0.94546E-01 Friction velocity uk : 0.21221E-11 0.94546E-01 Dimensionless distance yplus : 0.10611E-08 0.94546E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45926E-02 1438 0.89982E-08 0.40301E-05 0.88965E-01 c Velocity[X] 0.40301E-05 c Velocity[Y] 0.17855E-38 c Velocity[Z] 0.19253E-38 c Pressure 0.50436E-18 0 0.10000E+01 -0.50436E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0096289 0.91074 0.15075 0.15075 v Velocity[Y] -5.6345e-18 1.4001e-17 2.2639e-19 2.2639e-19 v Velocity[Z] -4.4991e-18 6.0201e-18 -6.4395e-22 -6.4395e-22 v ǁVelocityǁ 0.0096289 0.91074 0.15075 0.15075 v Pressure 0 0 0 0 v CourantNb 0 3.4158e-16 2.1637e-17 2.1637e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.341000000E+02 TIME STEP NUMBER 341 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18202E-11 0.94477E-01 Friction velocity uk : 0.18202E-11 0.94477E-01 Dimensionless distance yplus : 0.91008E-09 0.94477E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45952E-02 1438 0.89731E-08 0.40118E-05 0.88710E-01 c Velocity[X] 0.40118E-05 c Velocity[Y] 0.18467E-38 c Velocity[Z] 0.19120E-38 c Pressure 0.50474E-18 0 0.10000E+01 -0.50474E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0096142 0.91087 0.15082 0.15082 v Velocity[Y] -5.6549e-18 1.3985e-17 2.2507e-19 2.2507e-19 v Velocity[Z] -4.5037e-18 6.017e-18 -2.6703e-22 -2.6703e-22 v ǁVelocityǁ 0.0096142 0.91087 0.15082 0.15082 v Pressure 0 0 0 0 v CourantNb 0 3.4154e-16 2.166e-17 2.166e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.342000000E+02 TIME STEP NUMBER 342 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20082E-11 0.94409E-01 Friction velocity uk : 0.20082E-11 0.94409E-01 Dimensionless distance yplus : 0.10041E-08 0.94409E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.45979E-02 1437 0.90200E-08 0.39936E-05 0.88456E-01 c Velocity[X] 0.39936E-05 c Velocity[Y] 0.17328E-38 c Velocity[Z] 0.24083E-38 c Pressure 0.50517E-18 0 0.10000E+01 -0.50517E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0095995 0.911 0.15089 0.15089 v Velocity[Y] -5.6758e-18 1.3974e-17 2.2374e-19 2.2374e-19 v Velocity[Z] -4.51e-18 6.0346e-18 -3.8112e-22 -3.8112e-22 v ǁVelocityǁ 0.0095995 0.911 0.15089 0.15089 v Pressure 0 0 0 0 v CourantNb 0 3.4192e-16 2.1672e-17 2.1672e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.343000000E+02 TIME STEP NUMBER 343 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16976E-11 0.94341E-01 Friction velocity uk : 0.16976E-11 0.94341E-01 Dimensionless distance yplus : 0.84882E-09 0.94341E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46005E-02 1437 0.89950E-08 0.39756E-05 0.88203E-01 c Velocity[X] 0.39756E-05 c Velocity[Y] 0.15890E-38 c Velocity[Z] 0.16210E-38 c Pressure 0.50552E-18 0 0.10000E+01 -0.50552E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0095848 0.91113 0.15097 0.15097 v Velocity[Y] -5.6947e-18 1.3959e-17 2.2242e-19 2.2242e-19 v Velocity[Z] -4.4985e-18 5.9998e-18 -4.1487e-22 -4.1487e-22 v ǁVelocityǁ 0.0095848 0.91113 0.15097 0.15097 v Pressure 0 0 0 0 v CourantNb 0 3.4183e-16 2.1696e-17 2.1696e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.344000000E+02 TIME STEP NUMBER 344 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21231E-11 0.94273E-01 Friction velocity uk : 0.21231E-11 0.94273E-01 Dimensionless distance yplus : 0.10615E-08 0.94273E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46032E-02 1437 0.89702E-08 0.39576E-05 0.87952E-01 c Velocity[X] 0.39576E-05 c Velocity[Y] 0.18396E-38 c Velocity[Z] 0.19206E-38 c Pressure 0.50591E-18 0 0.10000E+01 -0.50591E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0095702 0.91125 0.15104 0.15104 v Velocity[Y] -5.7139e-18 1.3944e-17 2.2109e-19 2.2109e-19 v Velocity[Z] -4.5203e-18 6.015e-18 -5.4737e-22 -5.4737e-22 v ǁVelocityǁ 0.0095702 0.91125 0.15104 0.15104 v Pressure 0 0 0 0 v CourantNb 0 3.4275e-16 2.1709e-17 2.1709e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.345000000E+02 TIME STEP NUMBER 345 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18814E-11 0.94205E-01 Friction velocity uk : 0.18814E-11 0.94205E-01 Dimensionless distance yplus : 0.94072E-09 0.94205E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46058E-02 1436 0.90173E-08 0.39398E-05 0.87703E-01 c Velocity[X] 0.39398E-05 c Velocity[Y] 0.16735E-38 c Velocity[Z] 0.24642E-38 c Pressure 0.50640E-18 0 0.10000E+01 -0.50640E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0095557 0.91138 0.15111 0.15111 v Velocity[Y] -5.7319e-18 1.393e-17 2.1975e-19 2.1975e-19 v Velocity[Z] -4.5056e-18 6.0138e-18 -5.047e-22 -5.047e-22 v ǁVelocityǁ 0.0095557 0.91138 0.15111 0.15111 v Pressure 0 0 0 0 v CourantNb 0 3.4271e-16 2.1716e-17 2.1716e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.346000000E+02 TIME STEP NUMBER 346 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21164E-11 0.94138E-01 Friction velocity uk : 0.21164E-11 0.94138E-01 Dimensionless distance yplus : 0.10582E-08 0.94138E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46084E-02 1436 0.89925E-08 0.39222E-05 0.87454E-01 c Velocity[X] 0.39222E-05 c Velocity[Y] 0.16032E-38 c Velocity[Z] 0.20294E-38 c Pressure 0.50669E-18 0 0.10000E+01 -0.50669E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0095413 0.91151 0.15119 0.15119 v Velocity[Y] -5.7518e-18 1.3916e-17 2.1842e-19 2.1842e-19 v Velocity[Z] -4.5229e-18 5.9928e-18 -6.8397e-22 -6.8397e-22 v ǁVelocityǁ 0.0095413 0.91151 0.15119 0.15119 v Pressure 0 0 0 0 v CourantNb 0 3.4223e-16 2.1739e-17 2.1739e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.347000000E+02 TIME STEP NUMBER 347 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20655E-11 0.94071E-01 Friction velocity uk : 0.20655E-11 0.94071E-01 Dimensionless distance yplus : 0.10327E-08 0.94071E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46111E-02 1435 0.90399E-08 0.39047E-05 0.87208E-01 c Velocity[X] 0.39047E-05 c Velocity[Y] 0.15317E-38 c Velocity[Z] 0.15059E-38 c Pressure 0.50718E-18 0 0.10000E+01 -0.50718E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0095269 0.91163 0.15126 0.15126 v Velocity[Y] -5.7704e-18 1.3901e-17 2.1708e-19 2.1708e-19 v Velocity[Z] -4.5189e-18 5.9955e-18 -5.2582e-22 -5.2582e-22 v ǁVelocityǁ 0.0095269 0.91163 0.15126 0.15126 v Pressure 0 0 0 0 v CourantNb 0 3.4309e-16 2.1756e-17 2.1756e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.348000000E+02 TIME STEP NUMBER 348 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19763E-11 0.94004E-01 Friction velocity uk : 0.19763E-11 0.94004E-01 Dimensionless distance yplus : 0.98815E-09 0.94004E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46137E-02 1435 0.90152E-08 0.38872E-05 0.86962E-01 c Velocity[X] 0.38872E-05 c Velocity[Y] 0.16872E-38 c Velocity[Z] 0.24223E-38 c Pressure 0.50754E-18 0 0.10000E+01 -0.50754E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0095126 0.91176 0.15133 0.15133 v Velocity[Y] -5.7877e-18 1.3887e-17 2.1575e-19 2.1575e-19 v Velocity[Z] -4.5308e-18 5.9987e-18 -4.4711e-22 -4.4711e-22 v ǁVelocityǁ 0.0095126 0.91176 0.15133 0.15133 v Pressure 0 0 0 0 v CourantNb 0 3.4289e-16 2.1759e-17 2.1759e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.349000000E+02 TIME STEP NUMBER 349 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19827E-11 0.93938E-01 Friction velocity uk : 0.19827E-11 0.93938E-01 Dimensionless distance yplus : 0.99137E-09 0.93938E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46163E-02 1435 0.89907E-08 0.38700E-05 0.86718E-01 c Velocity[X] 0.38700E-05 c Velocity[Y] 0.17155E-38 c Velocity[Z] 0.19310E-38 c Pressure 0.50786E-18 0 0.10000E+01 -0.50786E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0094983 0.91188 0.1514 0.1514 v Velocity[Y] -5.8074e-18 1.3872e-17 2.144e-19 2.144e-19 v Velocity[Z] -4.5163e-18 5.9968e-18 -8.1912e-23 -8.1912e-23 v ǁVelocityǁ 0.0094983 0.91188 0.1514 0.1514 v Pressure 0 0 0 0 v CourantNb 0 3.4376e-16 2.1776e-17 2.1776e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.350000000E+02 TIME STEP NUMBER 350 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20924E-11 0.93871E-01 Friction velocity uk : 0.20924E-11 0.93871E-01 Dimensionless distance yplus : 0.10462E-08 0.93871E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46189E-02 1434 0.90382E-08 0.38528E-05 0.86475E-01 c Velocity[X] 0.38528E-05 c Velocity[Y] 0.17385E-38 c Velocity[Z] 0.20286E-38 c Pressure 0.50828E-18 0 0.10000E+01 -0.50828E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0094841 0.91201 0.15148 0.15148 v Velocity[Y] -5.8263e-18 1.3858e-17 2.1306e-19 2.1306e-19 v Velocity[Z] -4.5121e-18 6.0461e-18 -1.8587e-22 -1.8587e-22 v ǁVelocityǁ 0.0094841 0.91201 0.15148 0.15148 v Pressure 0 0 0 0 v CourantNb 0 3.4279e-16 2.1772e-17 2.1772e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.351000000E+02 TIME STEP NUMBER 351 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20005E-11 0.93805E-01 Friction velocity uk : 0.20005E-11 0.93805E-01 Dimensionless distance yplus : 0.10002E-08 0.93805E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46215E-02 1434 0.90137E-08 0.38358E-05 0.86234E-01 c Velocity[X] 0.38358E-05 c Velocity[Y] 0.17182E-38 c Velocity[Z] 0.20011E-38 c Pressure 0.50867E-18 0 0.10000E+01 -0.50867E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.00947 0.91213 0.15155 0.15155 v Velocity[Y] -5.8452e-18 1.3846e-17 2.1171e-19 2.1171e-19 v Velocity[Z] -4.5293e-18 6.0059e-18 -6.0446e-22 -6.0446e-22 v ǁVelocityǁ 0.00947 0.91213 0.15155 0.15155 v Pressure 0 0 0 0 v CourantNb 0 3.4326e-16 2.1804e-17 2.1804e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.352000000E+02 TIME STEP NUMBER 352 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17001E-11 0.93740E-01 Friction velocity uk : 0.17001E-11 0.93740E-01 Dimensionless distance yplus : 0.85003E-09 0.93740E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46241E-02 1434 0.89894E-08 0.38189E-05 0.85994E-01 c Velocity[X] 0.38189E-05 c Velocity[Y] 0.17493E-38 c Velocity[Z] 0.19051E-38 c Pressure 0.50901E-18 0 0.10000E+01 -0.50901E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0094559 0.91225 0.15162 0.15162 v Velocity[Y] -5.8642e-18 1.383e-17 2.1036e-19 2.1036e-19 v Velocity[Z] -4.5403e-18 6.0354e-18 -6.8625e-22 -6.8625e-22 v ǁVelocityǁ 0.0094559 0.91225 0.15162 0.15162 v Pressure 0 0 0 0 v CourantNb 0 3.4245e-16 2.1834e-17 2.1834e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.353000000E+02 TIME STEP NUMBER 353 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20594E-11 0.93674E-01 Friction velocity uk : 0.20594E-11 0.93674E-01 Dimensionless distance yplus : 0.10297E-08 0.93674E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46267E-02 1433 0.90371E-08 0.38021E-05 0.85756E-01 c Velocity[X] 0.38021E-05 c Velocity[Y] 0.16355E-38 c Velocity[Z] 0.16057E-38 c Pressure 0.50951E-18 0 0.10000E+01 -0.50951E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0094419 0.91237 0.15169 0.15169 v Velocity[Y] -5.8826e-18 1.3815e-17 2.0901e-19 2.0901e-19 v Velocity[Z] -4.511e-18 6.0347e-18 -6.4803e-22 -6.4803e-22 v ǁVelocityǁ 0.0094419 0.91237 0.15169 0.15169 v Pressure 0 0 0 0 v CourantNb 0 3.433e-16 2.185e-17 2.185e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.354000000E+02 TIME STEP NUMBER 354 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16374E-11 0.93609E-01 Friction velocity uk : 0.16374E-11 0.93609E-01 Dimensionless distance yplus : 0.81871E-09 0.93609E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46293E-02 1433 0.90128E-08 0.37854E-05 0.85518E-01 c Velocity[X] 0.37854E-05 c Velocity[Y] 0.19388E-38 c Velocity[Z] 0.21963E-38 c Pressure 0.50977E-18 0 0.10000E+01 -0.50977E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.009428 0.9125 0.15177 0.15177 v Velocity[Y] -5.9004e-18 1.3799e-17 2.0765e-19 2.0765e-19 v Velocity[Z] -4.5413e-18 6.0354e-18 -9.4475e-22 -9.4475e-22 v ǁVelocityǁ 0.009428 0.9125 0.15177 0.15177 v Pressure 0 0 0 0 v CourantNb 0 3.4382e-16 2.1846e-17 2.1846e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.355000000E+02 TIME STEP NUMBER 355 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15177E-11 0.93544E-01 Friction velocity uk : 0.15177E-11 0.93544E-01 Dimensionless distance yplus : 0.75885E-09 0.93544E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46319E-02 1433 0.89887E-08 0.37689E-05 0.85282E-01 c Velocity[X] 0.37689E-05 c Velocity[Y] 0.16910E-38 c Velocity[Z] 0.27274E-38 c Pressure 0.51027E-18 0 0.10000E+01 -0.51027E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0094141 0.91262 0.15184 0.15184 v Velocity[Y] -5.9178e-18 1.378e-17 2.0629e-19 2.0629e-19 v Velocity[Z] -4.5167e-18 6.0349e-18 -4.412e-22 -4.412e-22 v ǁVelocityǁ 0.0094141 0.91262 0.15184 0.15184 v Pressure 0 0 0 0 v CourantNb 0 3.432e-16 2.1886e-17 2.1886e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.356000000E+02 TIME STEP NUMBER 356 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15974E-11 0.93479E-01 Friction velocity uk : 0.15974E-11 0.93479E-01 Dimensionless distance yplus : 0.79868E-09 0.93479E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46344E-02 1432 0.90366E-08 0.37525E-05 0.85047E-01 c Velocity[X] 0.37525E-05 c Velocity[Y] 0.20580E-38 c Velocity[Z] 0.20973E-38 c Pressure 0.51064E-18 0 0.10000E+01 -0.51064E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0094002 0.91274 0.15191 0.15191 v Velocity[Y] -5.9372e-18 1.3763e-17 2.0492e-19 2.0492e-19 v Velocity[Z] -4.5374e-18 6.0187e-18 -8.2428e-22 -8.2428e-22 v ǁVelocityǁ 0.0094002 0.91274 0.15191 0.15191 v Pressure 0 0 0 0 v CourantNb 0 3.4408e-16 2.1885e-17 2.1885e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.357000000E+02 TIME STEP NUMBER 357 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11684E-11 0.93414E-01 Friction velocity uk : 0.11684E-11 0.93414E-01 Dimensionless distance yplus : 0.58420E-09 0.93414E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46370E-02 1432 0.90125E-08 0.37361E-05 0.84814E-01 c Velocity[X] 0.37361E-05 c Velocity[Y] 0.17301E-38 c Velocity[Z] 0.21245E-38 c Pressure 0.51100E-18 0 0.10000E+01 -0.51100E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0093865 0.91286 0.15198 0.15198 v Velocity[Y] -5.9568e-18 1.3748e-17 2.0355e-19 2.0355e-19 v Velocity[Z] -4.5176e-18 6.0473e-18 -1.2199e-21 -1.2199e-21 v ǁVelocityǁ 0.0093865 0.91286 0.15198 0.15198 v Pressure 0 0 0 0 v CourantNb 0 3.4394e-16 2.1918e-17 2.1918e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.358000000E+02 TIME STEP NUMBER 358 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11121E-11 0.93350E-01 Friction velocity uk : 0.11121E-11 0.93350E-01 Dimensionless distance yplus : 0.55603E-09 0.93350E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46396E-02 1432 0.89885E-08 0.37200E-05 0.84582E-01 c Velocity[X] 0.37200E-05 c Velocity[Y] 0.15481E-38 c Velocity[Z] 0.24388E-38 c Pressure 0.51138E-18 0 0.10000E+01 -0.51138E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0093727 0.91298 0.15205 0.15205 v Velocity[Y] -5.9745e-18 1.3734e-17 2.0218e-19 2.0218e-19 v Velocity[Z] -4.5502e-18 6.003e-18 -9.4859e-22 -9.4859e-22 v ǁVelocityǁ 0.0093727 0.91298 0.15205 0.15205 v Pressure 0 0 0 0 v CourantNb 0 3.4339e-16 2.1924e-17 2.1924e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.359000000E+02 TIME STEP NUMBER 359 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16214E-11 0.93286E-01 Friction velocity uk : 0.16214E-11 0.93286E-01 Dimensionless distance yplus : 0.81072E-09 0.93286E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46421E-02 1431 0.90367E-08 0.37039E-05 0.84351E-01 c Velocity[X] 0.37039E-05 c Velocity[Y] 0.17479E-38 c Velocity[Z] 0.23438E-38 c Pressure 0.51175E-18 0 0.10000E+01 -0.51175E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0093591 0.9131 0.15212 0.15212 v Velocity[Y] -5.9941e-18 1.3722e-17 2.0081e-19 2.0081e-19 v Velocity[Z] -4.534e-18 6.0369e-18 -8.0663e-22 -8.0663e-22 v ǁVelocityǁ 0.0093591 0.9131 0.15212 0.15212 v Pressure 0 0 0 0 v CourantNb 0 3.4497e-16 2.1927e-17 2.1927e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.360000000E+02 TIME STEP NUMBER 360 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19557E-11 0.93222E-01 Friction velocity uk : 0.19557E-11 0.93222E-01 Dimensionless distance yplus : 0.97786E-09 0.93222E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46447E-02 1431 0.90128E-08 0.36879E-05 0.84121E-01 c Velocity[X] 0.36879E-05 c Velocity[Y] 0.18847E-38 c Velocity[Z] 0.21030E-38 c Pressure 0.51221E-18 0 0.10000E+01 -0.51221E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0093455 0.91322 0.15219 0.15219 v Velocity[Y] -6.0127e-18 1.3705e-17 1.9943e-19 1.9943e-19 v Velocity[Z] -4.5268e-18 6.0312e-18 -1.4392e-21 -1.4392e-21 v ǁVelocityǁ 0.0093455 0.91322 0.15219 0.15219 v Pressure 0 0 0 0 v CourantNb 0 3.4419e-16 2.1959e-17 2.1959e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.361000000E+02 TIME STEP NUMBER 361 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13996E-11 0.93158E-01 Friction velocity uk : 0.13996E-11 0.93158E-01 Dimensionless distance yplus : 0.69979E-09 0.93158E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46472E-02 1431 0.89890E-08 0.36720E-05 0.83893E-01 c Velocity[X] 0.36720E-05 c Velocity[Y] 0.17875E-38 c Velocity[Z] 0.14250E-38 c Pressure 0.51248E-18 0 0.10000E+01 -0.51248E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0093319 0.91333 0.15227 0.15227 v Velocity[Y] -6.0322e-18 1.3688e-17 1.9804e-19 1.9804e-19 v Velocity[Z] -4.5334e-18 6.0492e-18 -9.9764e-22 -9.9764e-22 v ǁVelocityǁ 0.0093319 0.91333 0.15227 0.15227 v Pressure 0 0 0 0 v CourantNb 0 3.4404e-16 2.1978e-17 2.1978e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.362000000E+02 TIME STEP NUMBER 362 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16826E-11 0.93095E-01 Friction velocity uk : 0.16826E-11 0.93095E-01 Dimensionless distance yplus : 0.84128E-09 0.93095E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46498E-02 1430 0.90373E-08 0.36563E-05 0.83666E-01 c Velocity[X] 0.36563E-05 c Velocity[Y] 0.17522E-38 c Velocity[Z] 0.22359E-38 c Pressure 0.51294E-18 0 0.10000E+01 -0.51294E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0093184 0.91345 0.15234 0.15234 v Velocity[Y] -6.0509e-18 1.3672e-17 1.9666e-19 1.9666e-19 v Velocity[Z] -4.5149e-18 6.0453e-18 -7.6011e-22 -7.6011e-22 v ǁVelocityǁ 0.0093184 0.91345 0.15234 0.15234 v Pressure 0 0 0 0 v CourantNb 0 3.4483e-16 2.1987e-17 2.1987e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.363000000E+02 TIME STEP NUMBER 363 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16706E-11 0.93031E-01 Friction velocity uk : 0.16706E-11 0.93031E-01 Dimensionless distance yplus : 0.83531E-09 0.93031E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46523E-02 1430 0.90136E-08 0.36407E-05 0.83440E-01 c Velocity[X] 0.36407E-05 c Velocity[Y] 0.16806E-38 c Velocity[Z] 0.19378E-38 c Pressure 0.51325E-18 0 0.10000E+01 -0.51325E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.009305 0.91357 0.15241 0.15241 v Velocity[Y] -6.0689e-18 1.3658e-17 1.9527e-19 1.9527e-19 v Velocity[Z] -4.526e-18 6.031e-18 -9.5312e-22 -9.5312e-22 v ǁVelocityǁ 0.009305 0.91357 0.15241 0.15241 v Pressure 0 0 0 0 v CourantNb 0 3.4373e-16 2.198e-17 2.198e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.364000000E+02 TIME STEP NUMBER 364 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13226E-11 0.92968E-01 Friction velocity uk : 0.13226E-11 0.92968E-01 Dimensionless distance yplus : 0.66128E-09 0.92968E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46549E-02 1430 0.89900E-08 0.36251E-05 0.83215E-01 c Velocity[X] 0.36251E-05 c Velocity[Y] 0.17669E-38 c Velocity[Z] 0.21522E-38 c Pressure 0.51372E-18 0 0.10000E+01 -0.51372E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0092916 0.91369 0.15248 0.15248 v Velocity[Y] -6.0895e-18 1.3643e-17 1.9389e-19 1.9389e-19 v Velocity[Z] -4.5555e-18 6.0364e-18 -7.8547e-22 -7.8547e-22 v ǁVelocityǁ 0.0092916 0.91369 0.15248 0.15248 v Pressure 0 0 0 0 v CourantNb 0 3.4417e-16 2.2007e-17 2.2007e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.365000000E+02 TIME STEP NUMBER 365 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10958E-11 0.92906E-01 Friction velocity uk : 0.10958E-11 0.92906E-01 Dimensionless distance yplus : 0.54790E-09 0.92906E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46574E-02 1429 0.90385E-08 0.36097E-05 0.82991E-01 c Velocity[X] 0.36097E-05 c Velocity[Y] 0.18205E-38 c Velocity[Z] 0.18397E-38 c Pressure 0.51414E-18 0 0.10000E+01 -0.51414E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0092783 0.9138 0.15255 0.15255 v Velocity[Y] -6.1093e-18 1.3628e-17 1.9249e-19 1.9249e-19 v Velocity[Z] -4.5522e-18 6.0471e-18 -9.1357e-22 -9.1357e-22 v ǁVelocityǁ 0.0092783 0.9138 0.15255 0.15255 v Pressure 0 0 0 0 v CourantNb 0 3.4546e-16 2.2029e-17 2.2029e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.366000000E+02 TIME STEP NUMBER 366 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11578E-11 0.92843E-01 Friction velocity uk : 0.11578E-11 0.92843E-01 Dimensionless distance yplus : 0.57889E-09 0.92843E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46599E-02 1429 0.90150E-08 0.35944E-05 0.82769E-01 c Velocity[X] 0.35944E-05 c Velocity[Y] 0.16517E-38 c Velocity[Z] 0.16311E-38 c Pressure 0.51443E-18 0 0.10000E+01 -0.51443E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0092651 0.91392 0.15262 0.15262 v Velocity[Y] -6.1278e-18 1.3615e-17 1.911e-19 1.911e-19 v Velocity[Z] -4.5526e-18 6.0328e-18 -7.6765e-22 -7.6765e-22 v ǁVelocityǁ 0.0092651 0.91392 0.15262 0.15262 v Pressure 0 0 0 0 v CourantNb 0 3.4471e-16 2.2045e-17 2.2045e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.367000000E+02 TIME STEP NUMBER 367 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10110E-11 0.92781E-01 Friction velocity uk : 0.10110E-11 0.92781E-01 Dimensionless distance yplus : 0.50548E-09 0.92781E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46624E-02 1429 0.89915E-08 0.35792E-05 0.82548E-01 c Velocity[X] 0.35792E-05 c Velocity[Y] 0.17472E-38 c Velocity[Z] 0.14144E-38 c Pressure 0.51494E-18 0 0.10000E+01 -0.51494E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0092518 0.91403 0.15269 0.15269 v Velocity[Y] -6.1474e-18 1.36e-17 1.8971e-19 1.8971e-19 v Velocity[Z] -4.546e-18 6.0421e-18 -6.6549e-22 -6.6549e-22 v ǁVelocityǁ 0.0092518 0.91403 0.15269 0.15269 v Pressure 0 0 0 0 v CourantNb 0 3.4534e-16 2.207e-17 2.207e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.368000000E+02 TIME STEP NUMBER 368 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11351E-11 0.92719E-01 Friction velocity uk : 0.11351E-11 0.92719E-01 Dimensionless distance yplus : 0.56755E-09 0.92719E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46649E-02 1428 0.90403E-08 0.35641E-05 0.82328E-01 c Velocity[X] 0.35641E-05 c Velocity[Y] 0.18339E-38 c Velocity[Z] 0.19010E-38 c Pressure 0.51510E-18 0 0.10000E+01 -0.51510E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0092387 0.91415 0.15276 0.15276 v Velocity[Y] -6.1675e-18 1.3583e-17 1.8831e-19 1.8831e-19 v Velocity[Z] -4.543e-18 6.0512e-18 -8.2325e-22 -8.2325e-22 v ǁVelocityǁ 0.0092387 0.91415 0.15276 0.15276 v Pressure 0 0 0 0 v CourantNb 0 3.4537e-16 2.2075e-17 2.2075e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.369000000E+02 TIME STEP NUMBER 369 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17071E-11 0.92657E-01 Friction velocity uk : 0.17071E-11 0.92657E-01 Dimensionless distance yplus : 0.85356E-09 0.92657E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46674E-02 1428 0.90169E-08 0.35491E-05 0.82109E-01 c Velocity[X] 0.35491E-05 c Velocity[Y] 0.17569E-38 c Velocity[Z] 0.21104E-38 c Pressure 0.51562E-18 0 0.10000E+01 -0.51562E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0092256 0.91426 0.15283 0.15283 v Velocity[Y] -6.1859e-18 1.3568e-17 1.8691e-19 1.8691e-19 v Velocity[Z] -4.5554e-18 6.029e-18 -1.2749e-21 -1.2749e-21 v ǁVelocityǁ 0.0092256 0.91426 0.15283 0.15283 v Pressure 0 0 0 0 v CourantNb 0 3.4484e-16 2.2091e-17 2.2091e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.370000000E+02 TIME STEP NUMBER 370 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88128E-12 0.92595E-01 Friction velocity uk : 0.88128E-12 0.92595E-01 Dimensionless distance yplus : 0.44064E-09 0.92595E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46699E-02 1428 0.89936E-08 0.35342E-05 0.81892E-01 c Velocity[X] 0.35342E-05 c Velocity[Y] 0.16709E-38 c Velocity[Z] 0.21609E-38 c Pressure 0.51595E-18 0 0.10000E+01 -0.51595E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0092125 0.91438 0.1529 0.1529 v Velocity[Y] -6.2039e-18 1.3554e-17 1.8551e-19 1.8551e-19 v Velocity[Z] -4.55e-18 6.0269e-18 -9.2814e-22 -9.2814e-22 v ǁVelocityǁ 0.0092125 0.91438 0.1529 0.1529 v Pressure 0 0 0 0 v CourantNb 0 3.4635e-16 2.2086e-17 2.2086e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.371000000E+02 TIME STEP NUMBER 371 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13389E-11 0.92534E-01 Friction velocity uk : 0.13389E-11 0.92534E-01 Dimensionless distance yplus : 0.66947E-09 0.92534E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46724E-02 1428 0.89705E-08 0.35194E-05 0.81675E-01 c Velocity[X] 0.35194E-05 c Velocity[Y] 0.15800E-38 c Velocity[Z] 0.22315E-38 c Pressure 0.51623E-18 0 0.10000E+01 -0.51623E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0091995 0.91449 0.15297 0.15297 v Velocity[Y] -6.2222e-18 1.3544e-17 1.841e-19 1.841e-19 v Velocity[Z] -4.5492e-18 6.0439e-18 -7.7003e-22 -7.7003e-22 v ǁVelocityǁ 0.0091995 0.91449 0.15297 0.15297 v Pressure 0 0 0 0 v CourantNb 0 3.4544e-16 2.2096e-17 2.2096e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.372000000E+02 TIME STEP NUMBER 372 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19492E-11 0.92472E-01 Friction velocity uk : 0.19492E-11 0.92472E-01 Dimensionless distance yplus : 0.97459E-09 0.92472E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46749E-02 1427 0.90194E-08 0.35047E-05 0.81460E-01 c Velocity[X] 0.35047E-05 c Velocity[Y] 0.15557E-38 c Velocity[Z] 0.17465E-38 c Pressure 0.51680E-18 0 0.10000E+01 -0.51680E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0091866 0.9146 0.15304 0.15304 v Velocity[Y] -6.2404e-18 1.3529e-17 1.827e-19 1.827e-19 v Velocity[Z] -4.5448e-18 6.066e-18 -1e-21 -1e-21 v ǁVelocityǁ 0.0091866 0.9146 0.15304 0.15304 v Pressure 0 0 0 0 v CourantNb 0 3.4506e-16 2.2118e-17 2.2118e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.373000000E+02 TIME STEP NUMBER 373 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16706E-11 0.92411E-01 Friction velocity uk : 0.16706E-11 0.92411E-01 Dimensionless distance yplus : 0.83530E-09 0.92411E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46774E-02 1427 0.89963E-08 0.34901E-05 0.81245E-01 c Velocity[X] 0.34901E-05 c Velocity[Y] 0.17750E-38 c Velocity[Z] 0.21707E-38 c Pressure 0.51697E-18 0 0.10000E+01 -0.51697E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0091737 0.91471 0.15311 0.15311 v Velocity[Y] -6.259e-18 1.3515e-17 1.813e-19 1.813e-19 v Velocity[Z] -4.5513e-18 6.0528e-18 -9.0401e-22 -9.0401e-22 v ǁVelocityǁ 0.0091737 0.91471 0.15311 0.15311 v Pressure 0 0 0 0 v CourantNb 0 3.4555e-16 2.213e-17 2.213e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.374000000E+02 TIME STEP NUMBER 374 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13189E-11 0.92351E-01 Friction velocity uk : 0.13189E-11 0.92351E-01 Dimensionless distance yplus : 0.65943E-09 0.92351E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46799E-02 1427 0.89733E-08 0.34756E-05 0.81032E-01 c Velocity[X] 0.34756E-05 c Velocity[Y] 0.15248E-38 c Velocity[Z] 0.22448E-38 c Pressure 0.51744E-18 0 0.10000E+01 -0.51744E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0091609 0.91483 0.15318 0.15318 v Velocity[Y] -6.2782e-18 1.3503e-17 1.799e-19 1.799e-19 v Velocity[Z] -4.5461e-18 6.0751e-18 -8.3237e-22 -8.3237e-22 v ǁVelocityǁ 0.0091609 0.91483 0.15318 0.15318 v Pressure 0 0 0 0 v CourantNb 0 3.4478e-16 2.2152e-17 2.2152e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.375000000E+02 TIME STEP NUMBER 375 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17204E-11 0.92290E-01 Friction velocity uk : 0.17204E-11 0.92290E-01 Dimensionless distance yplus : 0.86018E-09 0.92290E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46824E-02 1426 0.90224E-08 0.34612E-05 0.80820E-01 c Velocity[X] 0.34612E-05 c Velocity[Y] 0.14640E-38 c Velocity[Z] 0.16767E-38 c Pressure 0.51772E-18 0 0.10000E+01 -0.51772E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0091481 0.91494 0.15325 0.15325 v Velocity[Y] -6.2967e-18 1.349e-17 1.785e-19 1.785e-19 v Velocity[Z] -4.5553e-18 6.06e-18 -8.9343e-22 -8.9343e-22 v ǁVelocityǁ 0.0091481 0.91494 0.15325 0.15325 v Pressure 0 0 0 0 v CourantNb 0 3.4583e-16 2.2152e-17 2.2152e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.376000000E+02 TIME STEP NUMBER 376 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15143E-11 0.92230E-01 Friction velocity uk : 0.15143E-11 0.92230E-01 Dimensionless distance yplus : 0.75713E-09 0.92230E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46848E-02 1426 0.89995E-08 0.34469E-05 0.80609E-01 c Velocity[X] 0.34469E-05 c Velocity[Y] 0.15965E-38 c Velocity[Z] 0.23508E-38 c Pressure 0.51817E-18 0 0.10000E+01 -0.51817E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0091353 0.91505 0.15332 0.15332 v Velocity[Y] -6.3155e-18 1.3477e-17 1.771e-19 1.771e-19 v Velocity[Z] -4.5442e-18 6.0582e-18 -6.4721e-22 -6.4721e-22 v ǁVelocityǁ 0.0091353 0.91505 0.15332 0.15332 v Pressure 0 0 0 0 v CourantNb 0 3.4539e-16 2.2168e-17 2.2168e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.377000000E+02 TIME STEP NUMBER 377 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17955E-11 0.92169E-01 Friction velocity uk : 0.17955E-11 0.92169E-01 Dimensionless distance yplus : 0.89776E-09 0.92169E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46873E-02 1426 0.89767E-08 0.34327E-05 0.80400E-01 c Velocity[X] 0.34327E-05 c Velocity[Y] 0.15475E-38 c Velocity[Z] 0.22101E-38 c Pressure 0.51860E-18 0 0.10000E+01 -0.51860E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0091227 0.91516 0.15339 0.15339 v Velocity[Y] -6.3334e-18 1.3464e-17 1.7571e-19 1.7571e-19 v Velocity[Z] -4.5521e-18 6.0626e-18 -8.0435e-22 -8.0435e-22 v ǁVelocityǁ 0.0091227 0.91516 0.15339 0.15339 v Pressure 0 0 0 0 v CourantNb 0 3.4506e-16 2.2195e-17 2.2195e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.378000000E+02 TIME STEP NUMBER 378 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14482E-11 0.92109E-01 Friction velocity uk : 0.14482E-11 0.92109E-01 Dimensionless distance yplus : 0.72411E-09 0.92109E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46898E-02 1425 0.90259E-08 0.34186E-05 0.80191E-01 c Velocity[X] 0.34186E-05 c Velocity[Y] 0.15976E-38 c Velocity[Z] 0.21412E-38 c Pressure 0.51894E-18 0 0.10000E+01 -0.51894E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.00911 0.91527 0.15346 0.15346 v Velocity[Y] -6.3521e-18 1.345e-17 1.7431e-19 1.7431e-19 v Velocity[Z] -4.5584e-18 6.0704e-18 -1.1509e-21 -1.1509e-21 v ǁVelocityǁ 0.00911 0.91527 0.15346 0.15346 v Pressure 0 0 0 0 v CourantNb 0 3.4655e-16 2.2211e-17 2.2211e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.379000000E+02 TIME STEP NUMBER 379 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11962E-11 0.92050E-01 Friction velocity uk : 0.11962E-11 0.92050E-01 Dimensionless distance yplus : 0.59811E-09 0.92050E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46922E-02 1425 0.90031E-08 0.34046E-05 0.79983E-01 c Velocity[X] 0.34046E-05 c Velocity[Y] 0.14935E-38 c Velocity[Z] 0.18660E-38 c Pressure 0.51919E-18 0 0.10000E+01 -0.51919E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0090974 0.91538 0.15353 0.15353 v Velocity[Y] -6.3697e-18 1.3437e-17 1.7292e-19 1.7292e-19 v Velocity[Z] -4.5573e-18 6.0517e-18 -8.7954e-22 -8.7954e-22 v ǁVelocityǁ 0.0090974 0.91538 0.15353 0.15353 v Pressure 0 0 0 0 v CourantNb 0 3.4731e-16 2.2234e-17 2.2234e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.380000000E+02 TIME STEP NUMBER 380 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13411E-11 0.91990E-01 Friction velocity uk : 0.13411E-11 0.91990E-01 Dimensionless distance yplus : 0.67054E-09 0.91990E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46947E-02 1425 0.89805E-08 0.33907E-05 0.79777E-01 c Velocity[X] 0.33907E-05 c Velocity[Y] 0.15641E-38 c Velocity[Z] 0.16409E-38 c Pressure 0.51968E-18 0 0.10000E+01 -0.51968E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0090849 0.91549 0.1536 0.1536 v Velocity[Y] -6.3881e-18 1.3421e-17 1.7152e-19 1.7152e-19 v Velocity[Z] -4.5656e-18 6.0472e-18 -7.8357e-22 -7.8357e-22 v ǁVelocityǁ 0.0090849 0.91549 0.1536 0.1536 v Pressure 0 0 0 0 v CourantNb 0 3.4584e-16 2.2236e-17 2.2236e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.381000000E+02 TIME STEP NUMBER 381 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12443E-11 0.91931E-01 Friction velocity uk : 0.12443E-11 0.91931E-01 Dimensionless distance yplus : 0.62215E-09 0.91931E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46971E-02 1424 0.90299E-08 0.33769E-05 0.79571E-01 c Velocity[X] 0.33769E-05 c Velocity[Y] 0.15441E-38 c Velocity[Z] 0.12821E-38 c Pressure 0.51998E-18 0 0.10000E+01 -0.51998E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0090724 0.9156 0.15367 0.15367 v Velocity[Y] -6.406e-18 1.3406e-17 1.7013e-19 1.7013e-19 v Velocity[Z] -4.5658e-18 6.0767e-18 -7.9929e-22 -7.9929e-22 v ǁVelocityǁ 0.0090724 0.9156 0.15367 0.15367 v Pressure 0 0 0 0 v CourantNb 0 3.4648e-16 2.2236e-17 2.2236e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.382000000E+02 TIME STEP NUMBER 382 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17780E-11 0.91872E-01 Friction velocity uk : 0.17780E-11 0.91872E-01 Dimensionless distance yplus : 0.88901E-09 0.91872E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.46996E-02 1424 0.90073E-08 0.33631E-05 0.79367E-01 c Velocity[X] 0.33631E-05 c Velocity[Y] 0.14830E-38 c Velocity[Z] 0.15999E-38 c Pressure 0.52033E-18 0 0.10000E+01 -0.52033E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.00906 0.9157 0.15374 0.15374 v Velocity[Y] -6.4238e-18 1.3394e-17 1.6874e-19 1.6874e-19 v Velocity[Z] -4.5652e-18 6.0864e-18 -8.6155e-22 -8.6155e-22 v ǁVelocityǁ 0.00906 0.9157 0.15374 0.15374 v Pressure 0 0 0 0 v CourantNb 0 3.468e-16 2.2255e-17 2.2255e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.383000000E+02 TIME STEP NUMBER 383 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17819E-11 0.91813E-01 Friction velocity uk : 0.17819E-11 0.91813E-01 Dimensionless distance yplus : 0.89093E-09 0.91813E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47020E-02 1424 0.89849E-08 0.33495E-05 0.79163E-01 c Velocity[X] 0.33495E-05 c Velocity[Y] 0.16308E-38 c Velocity[Z] 0.27328E-38 c Pressure 0.52071E-18 0 0.10000E+01 -0.52071E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0090476 0.91581 0.15381 0.15381 v Velocity[Y] -6.4421e-18 1.338e-17 1.6734e-19 1.6734e-19 v Velocity[Z] -4.5454e-18 6.045e-18 -8.0534e-22 -8.0534e-22 v ǁVelocityǁ 0.0090476 0.91581 0.15381 0.15381 v Pressure 0 0 0 0 v CourantNb 0 3.4703e-16 2.2283e-17 2.2283e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.384000000E+02 TIME STEP NUMBER 384 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15259E-11 0.91754E-01 Friction velocity uk : 0.15259E-11 0.91754E-01 Dimensionless distance yplus : 0.76294E-09 0.91754E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47044E-02 1423 0.90345E-08 0.33359E-05 0.78961E-01 c Velocity[X] 0.33359E-05 c Velocity[Y] 0.16065E-38 c Velocity[Z] 0.20846E-38 c Pressure 0.52112E-18 0 0.10000E+01 -0.52112E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0090353 0.91592 0.15388 0.15388 v Velocity[Y] -6.4602e-18 1.3364e-17 1.6595e-19 1.6595e-19 v Velocity[Z] -4.5602e-18 6.0908e-18 -9.0478e-22 -9.0478e-22 v ǁVelocityǁ 0.0090353 0.91592 0.15388 0.15388 v Pressure 0 0 0 0 v CourantNb 0 3.4631e-16 2.2309e-17 2.2309e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.385000000E+02 TIME STEP NUMBER 385 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16834E-11 0.91695E-01 Friction velocity uk : 0.16834E-11 0.91695E-01 Dimensionless distance yplus : 0.84171E-09 0.91695E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47069E-02 1423 0.90121E-08 0.33225E-05 0.78760E-01 c Velocity[X] 0.33225E-05 c Velocity[Y] 0.15941E-38 c Velocity[Z] 0.16333E-38 c Pressure 0.52153E-18 0 0.10000E+01 -0.52153E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.009023 0.91603 0.15394 0.15394 v Velocity[Y] -6.479e-18 1.3352e-17 1.6455e-19 1.6455e-19 v Velocity[Z] -4.5508e-18 6.0853e-18 -4.6435e-22 -4.6435e-22 v ǁVelocityǁ 0.009023 0.91603 0.15394 0.15394 v Pressure 0 0 0 0 v CourantNb 0 3.466e-16 2.2314e-17 2.2314e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.386000000E+02 TIME STEP NUMBER 386 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16568E-11 0.91637E-01 Friction velocity uk : 0.16568E-11 0.91637E-01 Dimensionless distance yplus : 0.82838E-09 0.91637E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47093E-02 1423 0.89897E-08 0.33091E-05 0.78559E-01 c Velocity[X] 0.33091E-05 c Velocity[Y] 0.15975E-38 c Velocity[Z] 0.27616E-38 c Pressure 0.52189E-18 0 0.10000E+01 -0.52189E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0090107 0.91613 0.15401 0.15401 v Velocity[Y] -6.4975e-18 1.3336e-17 1.6316e-19 1.6316e-19 v Velocity[Z] -4.5564e-18 6.0694e-18 -8.1513e-22 -8.1513e-22 v ǁVelocityǁ 0.0090107 0.91613 0.15401 0.15401 v Pressure 0 0 0 0 v CourantNb 0 3.4625e-16 2.2328e-17 2.2328e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.387000000E+02 TIME STEP NUMBER 387 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16118E-11 0.91579E-01 Friction velocity uk : 0.16118E-11 0.91579E-01 Dimensionless distance yplus : 0.80588E-09 0.91579E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47117E-02 1422 0.90395E-08 0.32958E-05 0.78360E-01 c Velocity[X] 0.32958E-05 c Velocity[Y] 0.14531E-38 c Velocity[Z] 0.34212E-38 c Pressure 0.52221E-18 0 0.10000E+01 -0.52221E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089985 0.91624 0.15408 0.15408 v Velocity[Y] -6.5148e-18 1.3328e-17 1.6177e-19 1.6177e-19 v Velocity[Z] -4.5496e-18 6.0822e-18 -8.1029e-22 -8.1029e-22 v ǁVelocityǁ 0.0089985 0.91624 0.15408 0.15408 v Pressure 0 0 0 0 v CourantNb 0 3.4732e-16 2.2325e-17 2.2325e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.388000000E+02 TIME STEP NUMBER 388 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16373E-11 0.91521E-01 Friction velocity uk : 0.16373E-11 0.91521E-01 Dimensionless distance yplus : 0.81864E-09 0.91521E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47141E-02 1422 0.90173E-08 0.32826E-05 0.78162E-01 c Velocity[X] 0.32826E-05 c Velocity[Y] 0.14318E-38 c Velocity[Z] 0.30474E-38 c Pressure 0.52275E-18 0 0.10000E+01 -0.52275E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089864 0.91634 0.15415 0.15415 v Velocity[Y] -6.5334e-18 1.3318e-17 1.6038e-19 1.6038e-19 v Velocity[Z] -4.5748e-18 6.0874e-18 -1.036e-21 -1.036e-21 v ǁVelocityǁ 0.0089864 0.91634 0.15415 0.15415 v Pressure 0 0 0 0 v CourantNb 0 3.4712e-16 2.2376e-17 2.2376e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.389000000E+02 TIME STEP NUMBER 389 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16365E-11 0.91463E-01 Friction velocity uk : 0.16365E-11 0.91463E-01 Dimensionless distance yplus : 0.81823E-09 0.91463E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47165E-02 1422 0.89951E-08 0.32695E-05 0.77964E-01 c Velocity[X] 0.32695E-05 c Velocity[Y] 0.14197E-38 c Velocity[Z] 0.38924E-38 c Pressure 0.52301E-18 0 0.10000E+01 -0.52301E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089743 0.91645 0.15422 0.15422 v Velocity[Y] -6.5518e-18 1.3307e-17 1.5899e-19 1.5899e-19 v Velocity[Z] -4.5479e-18 6.0802e-18 -5.3956e-22 -5.3956e-22 v ǁVelocityǁ 0.0089743 0.91645 0.15422 0.15422 v Pressure 0 0 0 0 v CourantNb 0 3.4815e-16 2.2379e-17 2.2379e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.390000000E+02 TIME STEP NUMBER 390 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16402E-11 0.91406E-01 Friction velocity uk : 0.16402E-11 0.91406E-01 Dimensionless distance yplus : 0.82011E-09 0.91406E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47189E-02 1422 0.89730E-08 0.32565E-05 0.77768E-01 c Velocity[X] 0.32565E-05 c Velocity[Y] 0.14618E-38 c Velocity[Z] 0.26407E-38 c Pressure 0.52345E-18 0 0.10000E+01 -0.52345E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089623 0.91656 0.15429 0.15429 v Velocity[Y] -6.5714e-18 1.3296e-17 1.5761e-19 1.5761e-19 v Velocity[Z] -4.5713e-18 6.1031e-18 -5.7165e-22 -5.7165e-22 v ǁVelocityǁ 0.0089623 0.91656 0.15429 0.15429 v Pressure 0 0 0 0 v CourantNb 0 3.476e-16 2.2409e-17 2.2409e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.391000000E+02 TIME STEP NUMBER 391 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16517E-11 0.91348E-01 Friction velocity uk : 0.16517E-11 0.91348E-01 Dimensionless distance yplus : 0.82583E-09 0.91348E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47213E-02 1421 0.90230E-08 0.32435E-05 0.77573E-01 c Velocity[X] 0.32435E-05 c Velocity[Y] 0.14794E-38 c Velocity[Z] 0.19132E-38 c Pressure 0.52369E-18 0 0.10000E+01 -0.52369E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089502 0.91666 0.15436 0.15436 v Velocity[Y] -6.5902e-18 1.3282e-17 1.5623e-19 1.5623e-19 v Velocity[Z] -4.5573e-18 6.0893e-18 -8.971e-22 -8.971e-22 v ǁVelocityǁ 0.0089502 0.91666 0.15436 0.15436 v Pressure 0 0 0 0 v CourantNb 0 3.4804e-16 2.2409e-17 2.2409e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.392000000E+02 TIME STEP NUMBER 392 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14205E-11 0.91291E-01 Friction velocity uk : 0.14205E-11 0.91291E-01 Dimensionless distance yplus : 0.71024E-09 0.91291E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47237E-02 1421 0.90009E-08 0.32307E-05 0.77379E-01 c Velocity[X] 0.32307E-05 c Velocity[Y] 0.14582E-38 c Velocity[Z] 0.20487E-38 c Pressure 0.52414E-18 0 0.10000E+01 -0.52414E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089383 0.91676 0.15442 0.15442 v Velocity[Y] -6.6083e-18 1.3271e-17 1.5485e-19 1.5485e-19 v Velocity[Z] -4.5528e-18 6.0963e-18 -6.6496e-22 -6.6496e-22 v ǁVelocityǁ 0.0089383 0.91676 0.15442 0.15442 v Pressure 0 0 0 0 v CourantNb 0 3.48e-16 2.2409e-17 2.2409e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.393000000E+02 TIME STEP NUMBER 393 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13651E-11 0.91234E-01 Friction velocity uk : 0.13651E-11 0.91234E-01 Dimensionless distance yplus : 0.68256E-09 0.91234E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47261E-02 1421 0.89790E-08 0.32179E-05 0.77185E-01 c Velocity[X] 0.32179E-05 c Velocity[Y] 0.14051E-38 c Velocity[Z] 0.25101E-38 c Pressure 0.52445E-18 0 0.10000E+01 -0.52445E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089264 0.91687 0.15449 0.15449 v Velocity[Y] -6.6252e-18 1.3258e-17 1.5347e-19 1.5347e-19 v Velocity[Z] -4.5496e-18 6.1061e-18 -7.6529e-22 -7.6529e-22 v ǁVelocityǁ 0.0089264 0.91687 0.15449 0.15449 v Pressure 0 0 0 0 v CourantNb 0 3.4748e-16 2.2437e-17 2.2437e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.394000000E+02 TIME STEP NUMBER 394 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14825E-11 0.91177E-01 Friction velocity uk : 0.14825E-11 0.91177E-01 Dimensionless distance yplus : 0.74124E-09 0.91177E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47285E-02 1420 0.90291E-08 0.32052E-05 0.76993E-01 c Velocity[X] 0.32052E-05 c Velocity[Y] 0.14175E-38 c Velocity[Z] 0.26358E-38 c Pressure 0.52487E-18 0 0.10000E+01 -0.52487E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089145 0.91697 0.15456 0.15456 v Velocity[Y] -6.6428e-18 1.3245e-17 1.5209e-19 1.5209e-19 v Velocity[Z] -4.566e-18 6.122e-18 -4.6883e-22 -4.6883e-22 v ǁVelocityǁ 0.0089145 0.91697 0.15456 0.15456 v Pressure 0 0 0 0 v CourantNb 0 3.4727e-16 2.2447e-17 2.2447e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.395000000E+02 TIME STEP NUMBER 395 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15436E-11 0.91121E-01 Friction velocity uk : 0.15436E-11 0.91121E-01 Dimensionless distance yplus : 0.77181E-09 0.91121E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47309E-02 1420 0.90073E-08 0.31926E-05 0.76801E-01 c Velocity[X] 0.31926E-05 c Velocity[Y] 0.14135E-38 c Velocity[Z] 0.26260E-38 c Pressure 0.52516E-18 0 0.10000E+01 -0.52516E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0089027 0.91707 0.15463 0.15463 v Velocity[Y] -6.6596e-18 1.3233e-17 1.5072e-19 1.5072e-19 v Velocity[Z] -4.5473e-18 6.1094e-18 -4.2028e-22 -4.2028e-22 v ǁVelocityǁ 0.0089027 0.91707 0.15463 0.15463 v Pressure 0 0 0 0 v CourantNb 0 3.4855e-16 2.2471e-17 2.2471e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.396000000E+02 TIME STEP NUMBER 396 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12942E-11 0.91064E-01 Friction velocity uk : 0.12942E-11 0.91064E-01 Dimensionless distance yplus : 0.64711E-09 0.91064E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47333E-02 1420 0.89855E-08 0.31800E-05 0.76611E-01 c Velocity[X] 0.31800E-05 c Velocity[Y] 0.14072E-38 c Velocity[Z] 0.28231E-38 c Pressure 0.52547E-18 0 0.10000E+01 -0.52547E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0088909 0.91718 0.1547 0.1547 v Velocity[Y] -6.6771e-18 1.3221e-17 1.4935e-19 1.4935e-19 v Velocity[Z] -4.5731e-18 6.106e-18 -1.7566e-22 -1.7566e-22 v ǁVelocityǁ 0.0088909 0.91718 0.1547 0.1547 v Pressure 0 0 0 0 v CourantNb 0 3.4801e-16 2.2482e-17 2.2482e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.397000000E+02 TIME STEP NUMBER 397 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15231E-11 0.91008E-01 Friction velocity uk : 0.15231E-11 0.91008E-01 Dimensionless distance yplus : 0.76156E-09 0.91008E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47357E-02 1419 0.90358E-08 0.31676E-05 0.76421E-01 c Velocity[X] 0.31676E-05 c Velocity[Y] 0.15380E-38 c Velocity[Z] 0.25441E-38 c Pressure 0.52604E-18 0 0.10000E+01 -0.52604E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0088792 0.91728 0.15476 0.15476 v Velocity[Y] -6.6957e-18 1.3209e-17 1.4797e-19 1.4797e-19 v Velocity[Z] -4.5626e-18 6.1041e-18 -8.3325e-22 -8.3325e-22 v ǁVelocityǁ 0.0088792 0.91728 0.15476 0.15476 v Pressure 0 0 0 0 v CourantNb 0 3.483e-16 2.2489e-17 2.2489e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.398000000E+02 TIME STEP NUMBER 398 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13475E-11 0.90952E-01 Friction velocity uk : 0.13475E-11 0.90952E-01 Dimensionless distance yplus : 0.67376E-09 0.90952E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47380E-02 1419 0.90141E-08 0.31552E-05 0.76232E-01 c Velocity[X] 0.31552E-05 c Velocity[Y] 0.13941E-38 c Velocity[Z] 0.18172E-38 c Pressure 0.52628E-18 0 0.10000E+01 -0.52628E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0088675 0.91738 0.15483 0.15483 v Velocity[Y] -6.713e-18 1.3197e-17 1.466e-19 1.466e-19 v Velocity[Z] -4.5502e-18 6.1037e-18 -4.0891e-22 -4.0891e-22 v ǁVelocityǁ 0.0088675 0.91738 0.15483 0.15483 v Pressure 0 0 0 0 v CourantNb 0 3.4816e-16 2.2517e-17 2.2517e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.399000000E+02 TIME STEP NUMBER 399 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14225E-11 0.90896E-01 Friction velocity uk : 0.14225E-11 0.90896E-01 Dimensionless distance yplus : 0.71124E-09 0.90896E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47404E-02 1419 0.89924E-08 0.31429E-05 0.76045E-01 c Velocity[X] 0.31429E-05 c Velocity[Y] 0.14991E-38 c Velocity[Z] 0.30823E-38 c Pressure 0.52670E-18 0 0.10000E+01 -0.52670E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0088559 0.91748 0.1549 0.1549 v Velocity[Y] -6.7311e-18 1.3185e-17 1.4522e-19 1.4522e-19 v Velocity[Z] -4.5699e-18 6.1098e-18 -3.8525e-22 -3.8525e-22 v ǁVelocityǁ 0.0088559 0.91748 0.1549 0.1549 v Pressure 0 0 0 0 v CourantNb 0 3.4789e-16 2.2522e-17 2.2522e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 INSTANT 0.400000000E+02 TIME STEP NUMBER 400 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 5100 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 100 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14321E-11 0.90840E-01 Friction velocity uk : 0.14321E-11 0.90840E-01 Dimensionless distance yplus : 0.71606E-09 0.90840E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 5100 Total number of wall faces : 5100 ------------------------------------------------------------ Write final restart files checkpoint at iteration 400, Physical time 0.40000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.47427E-02 1419 0.89709E-08 0.31307E-05 0.75858E-01 c Velocity[X] 0.31307E-05 c Velocity[Y] 0.14117E-38 c Velocity[Z] 0.25235E-38 c Pressure 0.52695E-18 0 0.10000E+01 -0.52695E-18 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a Local Time Step 0.00019998 2500 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0088443 0.91758 0.15497 0.15497 v Velocity[Y] -6.7485e-18 1.3174e-17 1.4385e-19 1.4385e-19 v Velocity[Z] -4.5553e-18 6.1073e-18 -1.8402e-22 -1.8402e-22 v ǁVelocityǁ 0.0088443 0.91758 0.15497 0.15497 v Pressure 0 0 0 0 v CourantNb 0 3.4852e-16 2.2528e-17 2.2528e-17 v FourierNb 250.03 500.05 490.05 490.05 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Local Time Step 0.01 0.01 0.01 0.01 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 250.03 500.05 490.05 490.05 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation