commande : ./cs_solver --param internalFan1 *************************************************************** (R) Code_Saturne Version 4.2.1 Copyright (C) 1998-2016 EDF S.A., France révision 4.2.1 build ven. 25 mars 2016 15:34:34 CET Version MPI 3.0 (Open MPI 1.8.3) 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. *************************************************************** Configuration locale du cas : Date : ven. 29 avril 2016 10:18:59 CEST Système : Linux 4.2.0-34-generic Machine : VM-CAO-S81-BA Processeur : model name : Intel(R) Xeon(R) CPU E5620 @ 2.40GHz Mémoire : 5121 Mo Utilisateur : jbl (jbl) Répertoire : /home/jbl/Documents/Test_saturne/InternalFan/internalFan1/RESU/20160429-1018 Threads OpenMP : 1 Processeurs/noeud : 4 méthode de lecture : entrées/sorties standard, accès série méthode d'écriture : entrées/sorties standard, accès série Bibliothèques externes pour le partitionnement : ParMETIS 4.0.3 PT-SCOTCH 6.0.3 Lecture des méta-données du fichier: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 6 (Nb variables ) NSCAL = 0 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 6 (Nb cell properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = 0.00000E+00 (Gravity y component ) GZ = 0.00000E+00 (Gravity z component ) ICORIO = 0 (Coriolis source terms ) -- Continuous phase: RO0 = 0.11786E+01 (Reference density ) VISCL0 = 0.18300E-04 (Ref. molecular dyn. visc. ) CP0 = 0.10172E+04 (Ref. specific heat ) ICP = 0 (> 0: variable CP (usphyv) ) P0 = 0.10132E+06 (Ref. total pressure ) PRED0 = 0.00000E+00 (Ref. reduced pressure ) T0 = 0.29315E+03 (Ref. temperature ) IROVAR = 0 (Density constant(0) or not(1) IVIVAR = 0 (Molec. visc cst.(0) or not(1) Initial reference point for pressure XYZP0 = 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------- ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION ---------------------------------------- ICAVIT = -1 (-1: single phase flow ) ( 0: no vap./cond. model ) ( 1: Merkle's model ) ----------------------------------------------------------- ** THERMAL MODEL ------------- --- Continuous phase: - Commons ITHERM = 0 (0: no thermal model ) (1: temperature ) (2: enthalpy ) (3: total energy ) ITPSCL = 0 (0: none ) (1: temperature in Kelvin ) (2: temperature in Celsius ) ISCALT = -1 (Thermal scalar number ) ** TURBULENCE ---------- --- Continuous phase: - Commons ITURB = 21 (Turbulence model ) IWALLF = 3 (wall function ) (0: disabled ) (1: one scale power law (forbidden for k-epsilon)) (2: one scale log law ) (3: two scales log law ) (4: scalable wall function ) (5: two scales V. Driest ) (6: two scales smooth/rough ) IWALLT = 0 (Exch. coeff. correlation ) (0: not activated ) (1: activated ) YPLULI = 0.23810E+01 (Limit Y+ ) IGRHOK = 0 (1: computed Grad(rho k) ) - Linear production k-epsilon (ITURB = 21) ALMAX = -0.99900E+03 (Characteristic length ) UREF = 0.10000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 0 (k-epsilon coupling mode ) IGRAKE = 1 (Account for gravity ) RELAXV = 0.10000E+01 for k (Relaxation) RELAXV = 0.10000E+01 for epsilon (Relaxation) - Rotation/curvature correction IRCCOR = 0 (0: desactivated ) (1: activated ) --- Constants - Commons XKAPPA = 0.42000E+00 (Von Karman constant ) CSTLOG = 0.52000E+01 (U+=Log(y+)/kappa +CSTLOG ) APOW = 0.83000E+01 (U+=APOW (y+)**BPOW (W&W law)) BPOW = 0.14286E+00 (U+=APOW (y+)**BPOW (W&W law)) - Linear production k-epsilon (ITURB = 21) Ce1 = 0.14400E+01 (Cepsilon 1: production coef.) CE2 = 0.19200E+01 (Cepsilon 2: dissipat. coef.) SIGMAK = 0.10000E+01 (Prandtl relative to k ) SIGMAE = 0.13000E+01 (Prandtl relative to epsilon ) CMU = 0.90000E-01 (Cmu constant ) ----------------------------------------------------------- ** SECONDARY VISCOSITY ------------------- --- Continuous phase: IVISSE = 1 (1: accounted for ) ----------------------------------------------------------- ** TIME STEPPING ------------- UNSTEADY ALGORITHM --- Time step parameters IDTVAR = 0 (0 cst; 1,2 var (t, t-space ) IPTLRO = 0 (1: rho-related DT clipping ) COUMAX = 0.10000E+01 (Maximum target CFL ) FOUMAX = 0.10000E+02 (Maximum target Fourier ) VARRDT = 0.10000E+00 (For var. DT, max. increase ) DTMIN = 0.10000E-02 (Minimum time step ) DTMAX = 0.10000E+02 (Maximum time step ) DTREF = 0.10000E-01 (Reference time step ) With a non-constant time step (IDTVAR = 1 or 2), when the value of COUMAX or FOUMAX is negative or zero, the associated time step limitation (for CFL and Fourier respectively) is ignored. --- Frozen velocity field ICCVFG = 0 (1: frozen velocity field ) --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Velocity 1 0.1000E+01 Pressure 0 0.1000E+01 k 1 0.1000E+01 epsilon 1 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 ) ----------------------------------------------------------- ** CONVECTION - DIFFUSION ---------------------- --------------------------------------------------------------------- Variable ICONV IDIFF IDIFFT ISCHCV ISSTPC BLENCV THETAV --------------------------------------------------------------------- Velocity 1 1 1 1 0 0.10E+01 0.10E+01 Pressure 0 1 1 1 0 0.00E+00 0.10E+01 k 1 1 1 1 0 0.00E+00 0.10E+01 epsilon 1 1 1 1 0 0.00E+00 0.10E+01 ------------------------------------------------------------- ICONV = 0 ou 1 (1 for convection active ) IDIFF = 0 ou 1 (1 for total diffusion active) IDIFFT = 0 ou 1 (1 for turbulent diff. active) ISCHCV = 0 ou 1 (SOLU or CD ) ISSTPC = 0 ou 1 (1: no slope test ) BLENCV = [0.;1.] (1-upwind proportion ) THETAV = [0.;1.] (0.5 Crank-Nicolson/AB ) (theta for convection- ) (diffusion terms uses ) ((1-theta).old+theta.new ) ----------------------------------------------------------- ** STOKES ------ IDILAT = 1 (1 : without unsteady term in the continuity equation 2 : with unsteady term in the continuity equation) IPOROS = 0 (0 : without porous media 1 : with porous media) IPHYDR = 0 (1: account for explicit balance between pressure gradient, gravity source terms, and head losses ) ICALHY = 0 (1: compute hydrastatic pressure for Dirichlet conditions for pressure on outlet ) IPRCO = 1 (1: pressure-continuity ) IPUCOU = 0 (1: reinforced U-P coupling ) NTERUP = 1 (n: n sweeps on navsto for velocity/pressure coupling ) -- Continuous phase: IREVMC = 0 (Velocity reconstruction mode) RELAXV = 0.10000E+01 for pressure (relaxation) ARAK = 0.10000E+01 (Arakawa factor ) 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 ) ----------------------------------------------------------- ** GRADIENTS CALCULATION --------------------- IMRGRA = 0 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ------------------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ------------------------------------------------------------------- Velocity 100 1 0.1000E-04 0.1000E-06 0.0000E+00 Pressure 100 2 0.1000E-04 0.1000E-06 0.0000E+00 k 100 1 0.1000E-04 0.1000E-06 0.0000E+00 epsilon 100 1 0.1000E-04 0.1000E-06 0.0000E+00 ----------------------------------------------------------- ------------------------------------------- Variable IRCFLU IMLIGR CLIMGR ------------------------------------------- Velocity 1 -1 0.1500E+01 Pressure 1 -1 0.1500E+01 k 1 -1 0.1500E+01 epsilon 1 -1 0.1500E+01 ----------------------------------- NSWRGR = (nb sweep gradient reconstr. ) NSWRSM = (nb sweep rhs reconstrcution ) EPSRGR = (grad. reconstruction prec. ) EPSRSM = (rhs reconstruction prec. ) EXTRAG = [0.;1.] (gradients extrapolation ) IRCFLU = 0 ou 1 (flow reconstruction ) IMLIGR = < 0, 0 ou 1 (gradient limitation method ) CLIMGR = > 1 ou 1 (gradient limitation coeff. ) ----------------------------------------------------------- ** FACE INTERPOLATION ------------------ IMVISF = 0 (0 arithmetic ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- ------------------------------------ Variable EPSILO IDIRCL ------------------------------------ Velocity 0.1000E-07 1 Pressure 0.1000E-07 1 k 0.1000E-07 1 epsilon 0.1000E-07 1 ------------------------------------ IRESOL = -1 (automatic solver choice ) IPOL*1000 + 0 (p conjuguate gradient ) 1 (Jacobi ) IPOL*1000 + 2 (bicgstab ) avec IPOL (preconditioning degree ) NITMAX = (max number of iterations ) 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 = 10 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 0 (Checkpoint frequency ) --- Post-processed variables Velocity Pressure k epsilon TurbVisc CourantNb FourierNb total_pressure Yplus -- -- --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) NCAPT = 5 (Number of probes ) NTHSAV = -1 (Checkpoint frequency ) Number Name Nb. probes (-1: all) 2 Velocity[X] -1 3 Velocity[Y] -1 4 Velocity[Z] -1 5 Pressure -1 6 k -1 7 epsilon -1 9 LamVisc -1 10 TurbVisc -1 11 CourantNb -1 12 FourierNb -1 13 total_pressure -1 -- -- -- --- Log files NTLIST = 1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 2 Velocity 0 5 Pressure 0 6 k 0 7 epsilon 0 10 TurbVisc -999 11 CourantNb -999 12 FourierNb -999 13 total_pressure -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 1 (Force exerted by the fluid on the 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) ----------------------------------------------------------- Gestionnaires de sorties pour post traitement : ----------------------------------------------- -1: nom: results répertoire: postprocessing format: EnSight Gold options: binary dépendence en temps: maillage fixe sorties: à la fin du calcul Lecture du fichier : mesh_input Fin de la lecture : mesh_input Nombre de cellules : 15625 ---------------------------------------------------------- Nombre de cellules + cellules halo : 15625 ---------------------------------------------------------- Nombre de faces internes : 45000 ---------------------------------------------------------- Nombre de faces de bord : 3750 ---------------------------------------------------------- Histogramme du nombre de faces internes par cellule : valeur minimale = 3 valeur maximale = 6 1 : [ 3 ; 4 [ = 8 2 : [ 4 ; 5 [ = 276 3 : [ 5 ; 6 ] = 15341 ---------------------------------------------------------- Renumérotation du maillage: renumérotation des cellules : pré-numérotation none cellules adjacentes aux halos en dernier : non numérotation : none renumérotation des faces internes : pré-ordonnancement par cellules adjacentes : id le plus bas en premier faces adjacentes aux halos en dernier : non numérotation : none renumérotation des faces de bord : numérotation : none ---------------------------------------------------------- Largeur de bande de la matrice pour maillage volumique : 625 Profil/lignes de la matrice pour le maillage volumique : 625 Coordonnées du maillage minimale et maximale X : 0.0000000e+00 5.0000000e-01 Y : 0.0000000e+00 5.0000000e-01 Z : 0.0000000e+00 5.0000000e-01 Maillage Nombre de cellules : 15625 Nombre de faces internes : 45000 Nombre de faces de bord : 3750 Nombre de sommets : 17576 Groupes : "Wall" faces de bord : 3750 --- Information sur les volumes Volume de controle minimal = 8.0000000e-06 Volume de controle maximal = 8.0000000e-06 Volume total du domaine = 1.2500000e-01 Critère 1 : orthogonalité : Nombre de mauvaises cellules détecté : 0 --> 0 % Critère 2 : décentrement : Nombre de mauvaises cellules détecté : 0 --> 0 % Critère 3 : qualité du gradient moindres-carrés : Nombre de mauvaises cellules détecté : 0 --> 0 % Critère 4 : ratio des volumes de cellules : Nombre de mauvaises cellules détecté : 0 --> 0 % Critère 5 : culpabilité par association : Nombre de mauvaises cellules détecté : 0 --> 0 % Computing geometric quantities (0.0415 s) ALMAX = 0.50000E+00 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 k 0.6000E-03 0.6000E-03 epsilon 0.2645E-05 0.2645E-05 --------------------------------- dt 0.1000E-01 0.1000E-01 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E-01 TIME STEP NUMBER 1 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1179E+01 0.1179E+01 molecular_viscos 0.1830E-04 0.1830E-04 turbulent_viscos 0.1444E-01 0.1444E-01 ----------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 0 Smooth wall 5 3750 Rough wall 6 0 Symmetry 4 0 Free outlet 3 0 Free inlet 13 0 Convective inlet 15 0 Free surface 14 0 Undefined 1 0 ------------------------------------------------------------------------- ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.11709E-01 0.11709E-01 Dimensionless distance yplus : 0.75413E+01 0.75413E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.80160E-04 31 0.49228E-08 0.58909E-07 0.41353E+01 c epsilon 0.45005E-04 33 0.38195E-08 0.10956E-04 0.99581E+02 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00051171 0.00059997 0.00058658 0.00058658 v epsilon 2.6452e-06 0.0018104 0.00017577 0.00017577 v TurbVisc 0.014435 0.014435 0.014435 0.014435 v CourantNb 0 0 0 0 v FourierNb 0.91972 1.8394 1.7659 1.7659 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 7.5413 7.5413 7.5413 7.5413 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.91972 1.8394 1.7659 1.7659 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.200000000E-01 TIME STEP NUMBER 2 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.10615E-01 0.11135E-01 Dimensionless distance yplus : 0.68369E+01 0.71714E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.69207E-04 20 0.42038E-08 0.11490E-08 0.57923E+00 c epsilon 0.39351E-04 19 0.31857E-08 0.77922E-08 0.27213E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00049378 0.00059995 0.00058475 0.00058475 v epsilon 2.645e-06 0.0016985 0.0001727 0.0001727 v TurbVisc 1.5342e-05 0.014435 0.0054648 0.0054648 v CourantNb 0 0 0 0 v FourierNb 0.0023647 1.8394 0.69749 0.69749 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 6.8369 7.1714 7.1327 7.1327 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023647 1.8394 0.69749 0.69749 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.300000000E-01 TIME STEP NUMBER 3 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.10383E-01 0.11058E-01 Dimensionless distance yplus : 0.66872E+01 0.71219E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.69003E-04 19 0.58901E-08 0.10914E-08 0.56614E+00 c epsilon 0.38403E-04 18 0.42938E-08 0.70599E-08 0.26528E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00047692 0.00059992 0.00058296 0.00058296 v epsilon 2.6448e-06 0.0015963 0.00016974 0.00016974 v TurbVisc 1.5227e-05 0.014435 0.0051992 0.0051992 v CourantNb 0 0 0 0 v FourierNb 0.0023566 1.8394 0.66369 0.66369 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 6.6872 7.1219 7.0734 7.0734 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023566 1.8394 0.66369 0.66369 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.400000000E-01 TIME STEP NUMBER 4 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.10161E-01 0.10982E-01 Dimensionless distance yplus : 0.65441E+01 0.70731E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.68805E-04 19 0.53690E-08 0.10377E-08 0.55360E+00 c epsilon 0.37498E-04 18 0.34983E-08 0.64162E-08 0.25886E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00046106 0.00059989 0.00058119 0.00058119 v epsilon 2.6447e-06 0.0015028 0.00016689 0.00016689 v TurbVisc 1.5115e-05 0.014435 0.0049807 0.0049807 v CourantNb 0 0 0 0 v FourierNb 0.0023486 1.8394 0.63588 0.63588 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 6.5441 7.0731 7.0153 7.0153 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023486 1.8394 0.63588 0.63588 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.500000000E-01 TIME STEP NUMBER 5 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.99485E-02 0.10908E-01 Dimensionless distance yplus : 0.64074E+01 0.70252E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.68611E-04 19 0.49696E-08 0.98759E-09 0.54155E+00 c epsilon 0.36633E-04 17 0.53485E-08 0.58480E-08 0.25285E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00044609 0.00059987 0.00057946 0.00057946 v epsilon 2.6446e-06 0.001417 0.00016413 0.00016413 v TurbVisc 1.5005e-05 0.014434 0.0047928 0.0047928 v CourantNb 0 0 0 0 v FourierNb 0.0023408 1.8393 0.61197 0.61197 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 6.4074 7.0252 6.9584 6.9584 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023408 1.8393 0.61197 0.61197 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.600000000E-01 TIME STEP NUMBER 6 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.97453E-02 0.10835E-01 Dimensionless distance yplus : 0.62765E+01 0.69781E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.68421E-04 19 0.46414E-08 0.94074E-09 0.52998E+00 c epsilon 0.35805E-04 17 0.46843E-08 0.53445E-08 0.24719E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00043196 0.00059984 0.00057775 0.00057775 v epsilon 2.6447e-06 0.0013381 0.00016146 0.00016146 v TurbVisc 1.4897e-05 0.014433 0.004627 0.004627 v CourantNb 0 0 0 0 v FourierNb 0.0023331 1.8392 0.59087 0.59087 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 6.2765 6.9781 6.9025 6.9025 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023331 1.8392 0.59087 0.59087 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.700000000E-01 TIME STEP NUMBER 7 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.95504E-02 0.10763E-01 Dimensionless distance yplus : 0.61510E+01 0.69317E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.68236E-04 19 0.43597E-08 0.89689E-09 0.51886E+00 c epsilon 0.35012E-04 17 0.41822E-08 0.48965E-08 0.24185E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00041859 0.00059981 0.00057606 0.00057606 v epsilon 2.6451e-06 0.0012655 0.00015888 0.00015888 v TurbVisc 1.4791e-05 0.014431 0.0044782 0.0044782 v CourantNb 0 0 0 0 v FourierNb 0.0023256 1.8389 0.57192 0.57192 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 6.151 6.9317 6.8478 6.8478 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023256 1.8389 0.57192 0.57192 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.800000000E-01 TIME STEP NUMBER 8 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.93635E-02 0.10692E-01 Dimensionless distance yplus : 0.60306E+01 0.68861E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.68055E-04 19 0.41109E-08 0.85579E-09 0.50815E+00 c epsilon 0.34251E-04 17 0.37866E-08 0.44967E-08 0.23682E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00040593 0.00059979 0.00057441 0.00057441 v epsilon 2.6457e-06 0.0011984 0.00015639 0.00015639 v TurbVisc 1.4687e-05 0.014428 0.0043428 0.0043428 v CourantNb 0 0 0 0 v FourierNb 0.0023182 1.8384 0.55469 0.55469 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 6.0306 6.8861 6.7941 6.7941 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023182 1.8384 0.55469 0.55469 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.900000000E-01 TIME STEP NUMBER 9 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.91840E-02 0.10622E-01 Dimensionless distance yplus : 0.59150E+01 0.68413E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.67878E-04 18 0.62292E-08 0.81721E-09 0.49783E+00 c epsilon 0.33521E-04 17 0.34650E-08 0.41386E-08 0.23205E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00039392 0.00059976 0.00057277 0.00057277 v epsilon 2.6468e-06 0.0011364 0.00015397 0.00015397 v TurbVisc 1.4585e-05 0.014423 0.0042185 0.0042185 v CourantNb 0 0 0 0 v FourierNb 0.0023109 1.8377 0.53888 0.53888 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 5.915 6.8413 6.7414 6.7414 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023109 1.8377 0.53888 0.53888 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 INSTANT 0.100000000E+00 TIME STEP NUMBER 10 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 3750 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Convective inlet 15 0 0.000000000E+00 Free surface 14 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.00000E+00 Friction velocity uk : 0.90115E-02 0.10554E-01 Dimensionless distance yplus : 0.58039E+01 0.67971E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 3750 ------------------------------------------------------------ Write final restart files checkpoint at iteration 10, Physical time 0.10000E+00 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: checkpoint/main End writing the options Variables principales écrites dans le fichier de reprise : 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 Coefficients de C.L. écrits dans le fichier de reprise : checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.67704E-04 18 0.59106E-08 0.78096E-09 0.48788E+00 c epsilon 0.32818E-04 17 0.31967E-08 0.38169E-08 0.22752E+01 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.00038252 0.00059973 0.00057116 0.00057116 v epsilon 2.6485e-06 0.0010789 0.00015162 0.00015162 v TurbVisc 1.4485e-05 0.014416 0.0041036 0.0041036 v CourantNb 0 0 0 0 v FourierNb 0.0023037 1.8367 0.52426 0.52426 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0133e+05 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 5.8039 6.7971 6.6897 6.6897 ** Valeurs calculées sur cellules ------------------------------ criterion minimum maximum moy. ensemble moy. spatiale --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0023037 1.8367 0.52426 0.52426 Fans ---- id surface volume flow deltaP ---- ----------- ----------- ----------- ----------- 0 4.0800e-02 5.0400e-04 0.0000e+00 6.0000e-01 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destruction des structures et clôture du calcul