commande : ./cs_solver *************************************************************** (R) Code_Saturne Version 6.0.8 Copyright (C) 1998-2019 EDF S.A., France révision 6.0.8-6e1ba748d build ven. 21 juin 2024 20:56:49 Version MPI 3.1 (Open MPI 4.1.2) 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 : dim. 23 juin 2024 12:17:21 Système : Linux 6.5.0-41-generic (Ubuntu 22.04.4 LTS) Machine : mrsm2p2itc-s16 Processeur : model name : Intel(R) Core(TM) i7-8700 CPU @ 3.20GHz Mémoire : 15811 Mo Utilisateur : friess (Christophe FRIESS) Répertoire : /home/friess/SIMUS/Code_Saturne/608/ICCFD/RANS/RESU/20240623-1217 Threads OpenMP : 1 Processeurs/noeud : 12 méthode de lecture : entrées/sorties standard, accès série méthode d'écriture : entrées/sorties standard, accès série 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 = 7 (Nb variables ) NSCAL = 0 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) ----------------------------------------------------------- ** HOMOGENEOUS MIXTURE MODEL VoF ---------------------------------------- IVOFMT = 0 ( 0 : disabled ) ( > 0: enabled ) ----------------------------------------------------------- ** TIME STEPPING ------------- ----------------------------------------------------------- ** STOKES ------ -- Continuous phase: 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 ) THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old THETCP = -0.99900E+03 (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 ) ----------------------------------------------------------- ** WALL DISTANCE COMPUTATION ------------------------- ICDPAR = 1 ( 1: std, reread if restart (-1: std, recomputed if restrt ( 2: old, reread if restart (-2: old, recomputed if restrt ----------------------------------------------------------- ** 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. NTPABS = 0 (Initial time step) NTMABS = 1000000 (Final time step required) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 0 (Checkpoint frequency ) --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) -- -- -- --- run_solver.log files NTLIST = 10000 (Output frequency ) -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 1 (Force exerted by the fluid on the boundary) ipstyp = 1 (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,2: CDO ) 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: text dépendence en temps: maillage fixe sorties: à la fin du calcul -5: nom: répertoire: monitoring format: time_plot options: dépendence en temps: maillage fixe sorties: tous les 1 pas de temps -6: nom: répertoire: profiles format: plot options: dépendence en temps: maillage fixe sorties: à la fin du calcul -7: nom: histograms répertoire: histograms format: histogram options: txt dépendence en temps: maillage fixe sorties: à la fin du calcul Lecture du fichier : mesh_input Fin de la lecture : mesh_input ------------------------------------------------------- Recollement numéro 1 : Type de périodicité : translation Matrice de transformation : 1 0 0 0.01 0 1 0 0 0 0 1 0 Critère de sélection : "x < 0.001 or x > 0.009" Paramètres de recollement : Fraction de la plus petite arête incidente : 0.10000 Angle maximum entre plans de faces recollées : 25.00000 Paramètres de recollement avancés : Niveau de verbosité : 1 Niveau de visualisation : 1 Profondeur max. pour construction de l'arbre : 30 Nombre max. de boîtes par feuille : 25 Rapport max. de boîtes liées / initiales : 5.00000 Rapport max. de boîtes pour la distribution : 2.00000 Multiplicateur de tolérance de fusion : 1.00000 Facteur pré-fusion : 0.05000 Mode de calcul de la tolérance : 1 Mode de calcul des intersections : 1 Nombre max. de suppressions d'équivalences : 500 Nombre max. de sous-faces par face : 200 Avant recollement Nombre de cellules : 27 Nombre de faces internes : 26 Nombre de faces de bord : 110 Nombre de sommets : 112 Nombre global de faces frontières sélectionnées pour le recollement : 54 Sélection d'éléments effectuée. Détermination des intersections possibles entre faces : répartition de l'arbre de boîtes englobantes : 2D Nombre global d'intersections détectées : 536 Intersections sommet-sommet : 536 Autres intersections : 0 L'opération de recollement est conforme. Intersections d'arêtes et création de sommets terminées. Pré-fusion pour 56 couples globaux d'éléments. Pas besoin de fusionner des sommets. Edge removed for 0 faces (global). Join mesh cleaning done. Edge removed for 0 faces (global). Join mesh cleaning done. Fusion de sommets et mise à jour du maillage terminées. Nombre global de faces après subdivision : 81 Global configuration after the joining operation: Global number of border faces to add: 0 Nettoyage du maillage pour des faces dégénérées. Nombre global de faces intérieures nettoyées : 0 Nombre global de faces de bord nettoyées : 0 Après recollement Nombre de cellules : 27 Nombre de faces internes : 80 Nombre de faces de bord : 56 Nombre de sommets : 112 Recollement 1 terminé (0.00109 s). ------------------------------------------------------- Recollement numéro 2 : Type de périodicité : translation Matrice de transformation : 1 0 0 0 0 1 0 0 0 0 1 0.01 Critère de sélection : "z < 0.001 or z >0.009" Paramètres de recollement : Fraction de la plus petite arête incidente : 0.10000 Angle maximum entre plans de faces recollées : 25.00000 Paramètres de recollement avancés : Niveau de verbosité : 1 Niveau de visualisation : 1 Profondeur max. pour construction de l'arbre : 30 Nombre max. de boîtes par feuille : 25 Rapport max. de boîtes liées / initiales : 5.00000 Rapport max. de boîtes pour la distribution : 2.00000 Multiplicateur de tolérance de fusion : 1.00000 Facteur pré-fusion : 0.05000 Mode de calcul de la tolérance : 1 Mode de calcul des intersections : 1 Nombre max. de suppressions d'équivalences : 500 Nombre max. de sous-faces par face : 200 Avant recollement Nombre de cellules : 27 Nombre de faces internes : 80 Nombre de faces de bord : 56 Nombre de sommets : 112 Nombre global de faces frontières sélectionnées pour le recollement : 54 Sélection d'éléments effectuée. Détermination des intersections possibles entre faces : répartition de l'arbre de boîtes englobantes : 2D Nombre global d'intersections détectées : 484 Intersections sommet-sommet : 484 Autres intersections : 0 L'opération de recollement est conforme. Intersections d'arêtes et création de sommets terminées. Pré-fusion pour 56 couples globaux d'éléments. Pas besoin de fusionner des sommets. Edge removed for 0 faces (global). Join mesh cleaning done. Edge removed for 0 faces (global). Join mesh cleaning done. Fusion de sommets et mise à jour du maillage terminées. Nombre global de faces après subdivision : 81 Global configuration after the joining operation: Global number of border faces to add: 0 Nettoyage du maillage pour des faces dégénérées. Nombre global de faces intérieures nettoyées : 0 Nombre global de faces de bord nettoyées : 0 Après recollement Nombre de cellules : 27 Nombre de faces internes : 134 Nombre de faces de bord : 2 Nombre de sommets : 112 Recollement 2 terminé (0.000877 s). Fin des étapes de recollement : Temps écoulé : 0.00205 ---------------------------------------------------------- Composition des périodicités Construction du halo avec voisinage standard ============================================ Création de l'interface entre faces Définition des sommets périodiques Création de l'interface entre sommets Création des halos Définition des halos Définition du halo local Création du halo distant Mise à jour de la connectivité faces -> cellules Nombre de cellules : 27 ---------------------------------------------------------- Nombre de cellules + cellules halo : 135 ---------------------------------------------------------- Nombre de cellules fantômes : 108 ---------------------------------------------------------- Nombre de faces internes : 134 ---------------------------------------------------------- Nombre de faces de bord : 2 ---------------------------------------------------------- Histogramme du nombre de faces internes par cellule : valeur minimale = 5 valeur maximale = 6 1 : [ 5 ; 6 ] = 27 ---------------------------------------------------------- Synchronisation des familles des cellules Écriture du fichier : mesh_output Fin de l'écriture : mesh_output Renumérotation du maillage: renumérotation des cellules : pré-numérotation pas de renumérotation cellules adjacentes aux halos en dernier : non numérotation : pas de renumérotation renumérotation des faces internes : pré-ordonnancement par cellules adjacentes : id le plus bas en premier faces adjacentes aux halos en dernier : non numérotation : multipasse renumérotation des faces de bord : numérotation : pas de cellule partagée entre fils renumérotation des sommets : numérotation : pas de renumérotation Numérotation pour cellules : type : défaut nombre d'éléments halo-adjacents : 27 Numérotation pour faces intérieures : type : défaut nombre d'éléments halo-adjacents : 134 Numérotation pour faces de bord : type : défaut nombre d'éléments halo-adjacents : 2 ---------------------------------------------------------- Largeur de bande de la matrice pour maillage volumique : 108 Profil/lignes de la matrice pour le maillage volumique : 108 Coordonnées du maillage minimale et maximale X : 0.0000000e+00 1.0000000e-02 Y : 0.0000000e+00 1.0000000e+00 Z : 0.0000000e+00 1.0000000e-02 Maillage Nombre de cellules : 27 Nombre de faces internes : 134 Nombre de faces de bord : 2 Nombre de sommets : 112 Faces périodiques (qui sont aussi des faces intérieures) : Périodicité 1 : 27 couples de faces Périodicité 2 : 27 couples de faces Groupes : "7" cellules : 27 faces intérieures : 108 faces de bord : 2 "PhysicalVolume29" cellules : 27 "xmax" faces intérieures : 27 "xmin" faces intérieures : 27 "ymax" faces de bord : 1 "ymin" faces de bord : 1 "zmax" faces intérieures : 27 "zmin" faces intérieures : 27 --- Information sur les volumes Volume de controle minimal = 4.9790736e-07 Volume de controle maximal = 1.1945051e-05 Volume total du domaine = 1.0000000e-04 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 (6.1e-05 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 27 Volume = 1.0000000e-04 Surface = -1 (not computed) Volume zone "all_cells" id = 1 Number of cells = 27 Volume = 1.0000000e-04 Surface = -1 (not computed) --- Information on boundary zones Zone de bord "boundary_faces" id = 0 Nombre de faces = 2 Surface = 2.0000000e-04 Perimeter = -1 (not computed) Zone de bord "BC_1" id = 1 Nombre de faces = 1 Surface = 1.0000000e-04 Perimeter = -1 (not computed) Zone de bord "BC_2" id = 2 Nombre de faces = 1 Surface = 1.0000000e-04 Perimeter = -1 (not computed) ALMAX = 0.46416E-01 (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 0.2000E+02 0.2000E+02 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 omega 0.5277E+00 0.5277E+00 Wall distance 0.0000E+00 0.0000E+00 --------------------------------- ------------------------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 0 Smooth wall 5 1 Rough wall 6 0 Symmetry 4 1 Free outlet 3 0 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E+01 TIME STEP NUMBER 1 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1000E+01 0.1000E+01 molecular_viscos 0.2550E-02 0.2550E-02 turbulent_viscos 0.1137E-02 0.1137E-02 ----------------------------------------- ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** WALL DISTANCE ------------- Min distance = 0.24926E-02 Max distance = 0.94206E+00 ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.77424E-01 8 0.49512E-08 0.12279E+06 0.15476E+05 c Velocity[X] 0.12279E+06 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 0.32975E-04 8 0.51735E-07 0.28722E-01 0.28240E+03 c omega 0.34963E+02 12 0.33717E-04 0.25188E-01 0.55579E+01 c Wall distance 0.25634E-04 16 0.98844E-08 0.99198E+02 0.29712E+03 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0024445 0.58169 0.21511 0.37425 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0.0024445 0.58169 0.21511 0.37425 v Pressure 0 0 0 0 v k 5.041e-07 0.015083 0.0043105 0.0087874 v omega 0.51883 0.51883 0.51883 0.51883 v TurbVisc 0.001137 0.001137 0.001137 0.001137 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 4.4192 2.2096 2.2096 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 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34348E-01 7 0.32935E-04 0.82882E-03 0.48363E+01 c Velocity[X] 0.82882E-03 c Velocity[Y] 0.81122E-36 c Velocity[Z] 0.16065E-68 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.24982E-03 8 0.17454E-07 0.71416E-07 0.17274E+01 c omega 0.33702E+02 10 0.11655E-03 0.19698E+12 0.38769E+04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0029198 0.58198 0.21556 0.37467 v Velocity[Y] -4.9299e-20 3.251e-20 -3.6848e-21 -2.4091e-21 v Velocity[Z] -7.1283e-36 -2.6612e-99 -2.7586e-37 -5.3476e-38 v ǁVelocityǁ 0.0029198 0.58198 0.21556 0.37467 v Pressure 0 0 0 0 v k 1.1456e-06 0.015083 0.0043139 0.0087904 v omega 0.51881 98548 4588.5 638.06 v TurbVisc 1.5918e-07 0.028557 0.0034732 0.0085137 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.048857 0.024429 0.024429 INSTANT 0.300000000E+01 TIME STEP NUMBER 3 ============================================================= ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11019E-01 8 0.18356E-05 0.66390E-02 0.48033E+01 c Velocity[X] 0.66390E-02 c Velocity[Y] 0.48390E-35 c Velocity[Z] 0.93433E-71 c Pressure 0.16941E-20 0 0.10000E+01 -0.16941E-20 0.00000E+00 c k 0.24993E-03 8 0.16205E-04 0.84175E-08 0.21995E+00 c omega 0.11430E+04 5 0.14670E+00 0.21414E+10 0.23855E+03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0046687 0.58271 0.22022 0.37798 v Velocity[Y] -2.8155e-19 1.8257e-19 -4.0231e-21 2.0253e-20 v Velocity[Z] -7.5245e-36 -1.2607e-76 -3.9878e-37 -7.7375e-38 v ǁVelocityǁ 0.0046687 0.58271 0.22022 0.37798 v Pressure 0 0 0 0 v k 5.9396e-07 0.015082 0.0043163 0.0087932 v omega 0.5188 75790 3584.9 500.71 v TurbVisc 1.1625e-11 0.028558 0.0034736 0.0085182 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.053396 0.026698 0.026698 INSTANT 0.400000000E+01 TIME STEP NUMBER 4 ============================================================= ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11072E-01 8 0.13421E-05 0.65732E-02 0.47721E+01 c Velocity[X] 0.65732E-02 c Velocity[Y] 0.74013E-35 c Velocity[Z] 0.25157E-70 c Pressure 0.16941E-20 0 0.10000E+01 -0.16941E-20 0.00000E+00 c k 0.25072E-03 8 0.68632E-05 0.81201E-08 0.21724E+00 c omega 0.69341E+03 5 0.13413E+00 0.11167E+10 0.21948E+03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0061042 0.58343 0.22483 0.38127 v Velocity[Y] -4.9549e-19 2.6952e-19 -1.1074e-21 1.9281e-20 v Velocity[Z] -7.8238e-36 -2.0066e-76 -5.0118e-37 -9.3022e-38 v ǁVelocityǁ 0.0061042 0.58343 0.22483 0.38127 v Pressure 0 0 0 0 v k 3.1223e-07 0.015081 0.0043186 0.0087959 v omega 0.51879 59378 2851 400 v TurbVisc 7.8369e-12 0.028559 0.0035033 0.0085806 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.06752 0.03376 0.03376 INSTANT 0.500000000E+01 TIME STEP NUMBER 5 ============================================================= ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11126E-01 8 0.15370E-05 0.65088E-02 0.47422E+01 c Velocity[X] 0.65088E-02 c Velocity[Y] 0.83558E-35 c Velocity[Z] 0.51258E-71 c Pressure 0.81566E-55 0 0.10000E+01 -0.81566E-55 0.00000E+00 c k 0.25152E-03 8 0.31224E-05 0.78703E-08 0.21502E+00 c omega 0.44128E+03 5 0.11610E+00 0.55432E+09 0.19161E+03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0073269 0.58415 0.22938 0.38453 v Velocity[Y] -4.9376e-19 5.4444e-19 8.9202e-21 1.8414e-20 v Velocity[Z] -8.0438e-36 -4.7821e-76 -5.87e-37 -1.1025e-37 v ǁVelocityǁ 0.0073269 0.58415 0.22938 0.38453 v Pressure 0 0 0 0 v k 1.6747e-07 0.01508 0.0043209 0.0087985 v omega 0.51877 47841 2325.2 327.63 v TurbVisc 5.2584e-12 0.02856 0.0035343 0.0086442 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.077205 0.038602 0.038602 INSTANT 0.600000000E+01 TIME STEP NUMBER 6 ============================================================= ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11181E-01 8 0.31410E-05 0.64470E-02 0.47131E+01 c Velocity[X] 0.64470E-02 c Velocity[Y] 0.46457E-35 c Velocity[Z] 0.32050E-70 c Pressure 0.33881E-20 0 0.10000E+01 -0.33881E-20 0.00000E+00 c k 0.25233E-03 8 0.15903E-05 0.76411E-08 0.21302E+00 c omega 0.30017E+03 5 0.93093E-01 0.25577E+09 0.15537E+03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0083999 0.58488 0.23389 0.38777 v Velocity[Y] -6.9412e-19 5.4445e-19 -2.4551e-20 -1.3495e-20 v Velocity[Z] -8.2404e-36 -7.159e-76 -6.5523e-37 -1.2888e-37 v ǁVelocityǁ 0.0083999 0.58488 0.23389 0.38777 v Pressure 0 0 0 0 v k 9.256e-08 0.015079 0.0043232 0.0088011 v omega 0.51876 40033 1959.9 277.15 v TurbVisc 3.5006e-12 0.028561 0.0035653 0.0087085 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.084585 0.042292 0.042292 INSTANT 0.700000000E+01 TIME STEP NUMBER 7 ============================================================= ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11236E-01 8 0.34424E-05 0.63863E-02 0.46847E+01 c Velocity[X] 0.63863E-02 c Velocity[Y] 0.69445E-35 c Velocity[Z] 0.60792E-70 c Pressure 0.33881E-20 0 0.10000E+01 -0.33881E-20 0.00000E+00 c k 0.25316E-03 8 0.94148E-06 0.74256E-08 0.21116E+00 c omega 0.22160E+03 5 0.67928E-01 0.10718E+09 0.11493E+03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0093635 0.58561 0.23834 0.39097 v Velocity[Y] -1.1316e-18 5.6252e-19 -3.4825e-20 -9.7087e-21 v Velocity[Z] -8.3619e-36 -1.2923e-75 -7.2246e-37 -1.5055e-37 v ǁVelocityǁ 0.0093635 0.58561 0.23834 0.39097 v Pressure 0 0 0 0 v k 5.3519e-08 0.015078 0.0043253 0.0088036 v omega 0.51875 35009 1716 243.29 v TurbVisc 2.3121e-12 0.028563 0.003597 0.0087738 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.090567 0.045283 0.045283 INSTANT 0.800000000E+01 TIME STEP NUMBER 8 ============================================================= ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11292E-01 8 0.20673E-05 0.63261E-02 0.46569E+01 c Velocity[X] 0.63261E-02 c Velocity[Y] 0.29740E-35 c Velocity[Z] 0.36834E-70 c Pressure 0.33881E-20 0 0.10000E+01 -0.33881E-20 0.00000E+00 c k 0.25400E-03 8 0.64654E-06 0.72200E-08 0.20941E+00 c omega 0.17826E+03 5 0.44854E-01 0.40273E+08 0.77076E+02 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.010244 0.58633 0.24275 0.39415 v Velocity[Y] -1.1316e-18 5.6212e-19 -4.2074e-20 -9.9497e-21 v Velocity[Z] -1.0766e-35 1.296e-36 -8.1125e-37 -1.7544e-37 v ǁVelocityǁ 0.010244 0.58633 0.24275 0.39415 v Pressure 0 0 0 0 v k 3.3059e-08 0.015077 0.0043274 0.008806 v omega 0.51873 31959 1560.3 221.54 v TurbVisc 1.5287e-12 0.028564 0.0036296 0.0088401 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.09562 0.04781 0.04781 INSTANT 0.900000000E+01 TIME STEP NUMBER 9 ============================================================= ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11349E-01 8 0.22249E-05 0.62665E-02 0.46296E+01 c Velocity[X] 0.62665E-02 c Velocity[Y] 0.83904E-35 c Velocity[Z] 0.99957E-68 c Pressure 0.33881E-20 0 0.10000E+01 -0.33881E-20 0.00000E+00 c k 0.25485E-03 8 0.49490E-06 0.70222E-08 0.20775E+00 c omega 0.15471E+03 5 0.27085E-01 0.13661E+08 0.47355E+02 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011061 0.58706 0.24711 0.3973 v Velocity[Y] -9.3197e-19 7.4343e-19 -2.0676e-20 1.5704e-20 v Velocity[Z] -8.9305e-36 4.7897e-35 1.9367e-36 3.4174e-37 v ǁVelocityǁ 0.011061 0.58706 0.24711 0.3973 v Pressure 0 0 0 0 v k 2.2307e-08 0.015076 0.0043295 0.0088084 v omega 0.51871 30210 1464.8 208.1 v TurbVisc 1.0344e-12 0.028565 0.003663 0.0089075 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.10002 0.050009 0.050009 INSTANT 0.100000000E+02 TIME STEP NUMBER 10 ============================================================= ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11407E-01 8 0.42657E-05 0.62090E-02 0.46027E+01 c Velocity[X] 0.62090E-02 c Velocity[Y] 0.10739E-34 c Velocity[Z] 0.37395E-67 c Pressure 0.13051E-53 0 0.10000E+01 -0.13051E-53 0.00000E+00 c k 0.25571E-03 8 0.40519E-06 0.68308E-08 0.20616E+00 c omega 0.14214E+03 5 0.15285E-01 0.42897E+07 0.27256E+02 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.011826 0.58779 0.25144 0.40042 v Velocity[Y] -7.2488e-19 7.4382e-19 -6.0127e-20 -1.0687e-20 v Velocity[Z] -6.322e-35 3.2528e-36 -3.1086e-36 -6.4253e-37 v ǁVelocityǁ 0.011826 0.58779 0.25144 0.40042 v Pressure 0 0 0 0 v k 1.6659e-08 0.015075 0.0043315 0.0088107 v omega 0.5187 29252 1408.1 200.03 v TurbVisc 7.384e-13 0.028566 0.0036961 0.0089756 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.10393 0.051963 0.051963 INSTANT 0.100000000E+05 TIME STEP NUMBER 10000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57513E+00 0.57513E+00 Friction velocity uk : 0.57513E+00 0.57513E+00 Dimensionless distance yplus : 0.56160E+00 0.56160E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44298E+00 5 0.47840E-07 0.63036E-03 0.15079E+00 c Velocity[X] 0.63036E-03 c Velocity[Y] 0.21381E-32 c Velocity[Z] 0.58276E-65 c Pressure 0.21684E-18 0 0.10000E+01 -0.21684E-18 0.00000E+00 c k 0.77640E-02 8 0.36442E-06 0.59505E-05 0.47203E+00 c omega 0.12895E+03 3 0.91470E-08 0.29406E-02 0.12355E-02 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.32301 10.628 7.2589 9.4393 v Velocity[Y] -7.3082e-17 2.599e-17 -1.154e-17 2.0485e-19 v Velocity[Z] -1.3974e-32 3.2508e-37 -2.3852e-33 -5.1648e-34 v ǁVelocityǁ 0.32301 10.628 7.2589 9.4393 v Pressure 0 0 0 0 v k 5.598e-05 0.60404 0.29705 0.21639 v omega 2.5956 28195 1369 208.38 v TurbVisc 1.9851e-09 0.017668 0.0092443 0.012777 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.5616 0.2808 0.2808 INSTANT 0.200000000E+05 TIME STEP NUMBER 20000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70816E+00 0.70816E+00 Friction velocity uk : 0.70816E+00 0.70816E+00 Dimensionless distance yplus : 0.69150E+00 0.69150E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10754E+01 4 0.10816E-06 0.17814E-03 0.82746E-01 c Velocity[X] 0.17814E-03 c Velocity[Y] 0.69098E-32 c Velocity[Z] 0.25345E-66 c Pressure 0.33881E-20 0 0.10000E+01 -0.33881E-20 0.00000E+00 c k 0.42873E-01 7 0.70184E-07 0.10424E-04 0.33639E+00 c omega 0.12918E+03 2 0.10164E-07 0.12873E-02 0.80414E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.48971 14.382 9.4464 12.227 v Velocity[Y] -1.2161e-16 6.6834e-17 -1.9183e-17 7.8893e-18 v Velocity[Z] -2.3508e-32 -2.3561e-69 -3.373e-33 -7.268e-34 v ǁVelocityǁ 0.48971 14.382 9.4464 12.227 v Pressure 0 0 0 0 v k 0.00020911 1.1389 0.72569 0.67279 v omega 6.6935 28194 1382.6 215.01 v TurbVisc 7.4163e-09 0.046973 0.023337 0.036213 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.6915 0.34575 0.34575 INSTANT 0.300000000E+05 TIME STEP NUMBER 30000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78800E+00 0.78800E+00 Friction velocity uk : 0.78800E+00 0.78800E+00 Dimensionless distance yplus : 0.76946E+00 0.76946E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.17464E+01 3 0.10354E-06 0.71930E-04 0.56969E-01 c Velocity[X] 0.71930E-04 c Velocity[Y] 0.11088E-31 c Velocity[Z] 0.89074E-66 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.76785E-01 6 0.20963E-07 0.66997E-06 0.67422E-01 c omega 0.12935E+03 2 0.68819E-08 0.47374E-03 0.60503E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.60634 15.278 10.655 13.487 v Velocity[Y] -1.3347e-16 5.7366e-17 -1.3704e-17 8.4242e-18 v Velocity[Z] -1.0475e-32 2.3641e-34 -1.3817e-33 -2.9601e-34 v ǁVelocityǁ 0.60634 15.278 10.655 13.487 v Pressure 0 0 0 0 v k 0.00038849 1.4854 0.96301 0.89913 v omega 5.8534 28194 1390.4 216.41 v TurbVisc 1.3779e-08 0.084709 0.035094 0.060577 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.76946 0.38473 0.38473 INSTANT 0.400000000E+05 TIME STEP NUMBER 40000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82812E+00 0.82812E+00 Friction velocity uk : 0.82812E+00 0.82812E+00 Dimensionless distance yplus : 0.80865E+00 0.80865E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.20096E+01 3 0.79207E-07 0.45580E-04 0.45693E-01 c Velocity[X] 0.45580E-04 c Velocity[Y] 0.11128E-31 c Velocity[Z] 0.24450E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.89375E-01 6 0.14637E-07 0.83847E-06 0.75268E-01 c omega 0.12944E+03 2 0.45465E-08 0.19910E-03 0.39584E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.66966 16.087 11.343 14.29 v Velocity[Y] -1.3831e-16 2.6551e-17 -4.069e-17 -2.3477e-17 v Velocity[Z] -3.2379e-33 1.3248e-32 1.3928e-33 2.072e-34 v ǁVelocityǁ 0.66966 16.087 11.343 14.29 v Pressure 0 0 0 0 v k 0.0005158 1.6771 1.0803 0.98866 v omega 5.6396 28194 1395 217.74 v TurbVisc 1.8295e-08 0.096699 0.037962 0.066185 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.80865 0.40432 0.40432 INSTANT 0.500000000E+05 TIME STEP NUMBER 50000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85841E+00 0.85841E+00 Friction velocity uk : 0.85841E+00 0.85841E+00 Dimensionless distance yplus : 0.83822E+00 0.83822E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.22138E+01 3 0.60517E-07 0.30300E-04 0.36686E-01 c Velocity[X] 0.30300E-04 c Velocity[Y] 0.11030E-31 c Velocity[Z] 0.24068E-63 c Pressure 0.21684E-18 0 0.10000E+01 -0.21684E-18 0.00000E+00 c k 0.10443E+00 6 0.11443E-07 0.88931E-06 0.75153E-01 c omega 0.12951E+03 2 0.40894E-08 0.13863E-03 0.34721E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.71954 16.786 11.864 14.915 v Velocity[Y] -1.3905e-16 4.8272e-17 -4.0588e-17 -2.224e-17 v Velocity[Z] -4.2836e-34 2.182e-32 3.7892e-33 8.118e-34 v ǁVelocityǁ 0.71954 16.786 11.864 14.915 v Pressure 0 0 0 0 v k 0.00063285 1.8341 1.1942 1.0934 v omega 5.8859 28194 1398.5 219.03 v TurbVisc 2.2446e-08 0.103 0.040354 0.070333 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.83822 0.41911 0.41911 INSTANT 0.600000000E+05 TIME STEP NUMBER 60000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88273E+00 0.88273E+00 Friction velocity uk : 0.88273E+00 0.88273E+00 Dimensionless distance yplus : 0.86197E+00 0.86197E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.23935E+01 2 0.18069E-06 0.18502E-04 0.28356E-01 c Velocity[X] 0.18502E-04 c Velocity[Y] 0.63356E-32 c Velocity[Z] 0.24175E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.11914E+00 6 0.83214E-08 0.61667E-06 0.59619E-01 c omega 0.12958E+03 2 0.33043E-08 0.86139E-04 0.27480E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.7609 17.333 12.279 15.407 v Velocity[Y] -1.3609e-16 6.8934e-17 -5.3151e-17 -2.2472e-17 v Velocity[Z] -1.6267e-32 4.4773e-33 -1.8646e-34 -2.8534e-36 v ǁVelocityǁ 0.7609 17.333 12.279 15.407 v Pressure 0 0 0 0 v k 0.00074109 1.9641 1.2919 1.187 v omega 6.1583 28194 1401.3 220.07 v TurbVisc 2.6285e-08 0.10882 0.042493 0.074114 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.86197 0.43099 0.43099 INSTANT 0.700000000E+05 TIME STEP NUMBER 70000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90162E+00 0.90162E+00 Friction velocity uk : 0.90162E+00 0.90162E+00 Dimensionless distance yplus : 0.88042E+00 0.88042E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.25400E+01 2 0.14435E-06 0.12842E-04 0.23452E-01 c Velocity[X] 0.12842E-04 c Velocity[Y] 0.78252E-32 c Velocity[Z] 0.19360E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.13149E+00 6 0.62414E-08 0.40821E-06 0.46408E-01 c omega 0.12962E+03 2 0.27579E-08 0.60665E-04 0.23019E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.7938 17.759 12.605 15.793 v Velocity[Y] -1.3221e-16 7.94e-17 -4.3101e-17 -1.6318e-17 v Velocity[Z] -3.7404e-34 2.469e-32 2.6959e-33 5.3022e-34 v ǁVelocityǁ 0.7938 17.759 12.605 15.793 v Pressure 0 0 0 0 v k 0.00083381 2.0674 1.3695 1.2615 v omega 6.3665 28194 1403.6 220.88 v TurbVisc 2.9574e-08 0.11354 0.044168 0.077104 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.88042 0.44021 0.44021 INSTANT 0.800000000E+05 TIME STEP NUMBER 80000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91693E+00 0.91693E+00 Friction velocity uk : 0.91693E+00 0.91693E+00 Dimensionless distance yplus : 0.89536E+00 0.89536E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.26609E+01 2 0.11747E-06 0.90676E-05 0.19586E-01 c Velocity[X] 0.90676E-05 c Velocity[Y] 0.72930E-32 c Velocity[Z] 0.13488E-65 c Pressure 0.21684E-18 0 0.10000E+01 -0.21684E-18 0.00000E+00 c k 0.14183E+00 5 0.71250E-08 0.29110E-06 0.37852E-01 c omega 0.12966E+03 2 0.23445E-08 0.42612E-04 0.19516E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.82099 18.11 12.874 16.112 v Velocity[Y] -1.426e-16 7.4179e-17 -5.8765e-17 -3.6372e-17 v Velocity[Z] -3.189e-35 1.009e-32 1.9218e-33 4.4668e-34 v ǁVelocityǁ 0.82099 18.11 12.874 16.112 v Pressure 0 0 0 0 v k 0.00091477 2.1527 1.4335 1.3224 v omega 6.5277 28194 1405.5 221.55 v TurbVisc 3.2446e-08 0.11721 0.045485 0.079444 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.89536 0.44768 0.44768 INSTANT 0.900000000E+05 TIME STEP NUMBER 90000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92966E+00 0.92966E+00 Friction velocity uk : 0.92966E+00 0.92966E+00 Dimensionless distance yplus : 0.90780E+00 0.90780E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.27639E+01 2 0.96390E-07 0.64482E-05 0.16425E-01 c Velocity[X] 0.64482E-05 c Velocity[Y] 0.71411E-32 c Velocity[Z] 0.70916E-66 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.15083E+00 5 0.58541E-08 0.21929E-06 0.32049E-01 c omega 0.12970E+03 2 0.21733E-08 0.38401E-04 0.18731E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.84394 18.403 13.097 16.376 v Velocity[Y] -1.3188e-16 5.5285e-17 -4.7134e-17 -3.2875e-17 v Velocity[Z] -1.0825e-36 1.6771e-32 2.3307e-33 5.2284e-34 v ǁVelocityǁ 0.84394 18.403 13.097 16.376 v Pressure 0 0 0 0 v k 0.00098687 2.2248 1.4877 1.374 v omega 6.6563 28194 1407 222.1 v TurbVisc 3.5003e-08 0.12028 0.046587 0.081403 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.9078 0.4539 0.4539 INSTANT 0.100000000E+06 TIME STEP NUMBER 100000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94033E+00 0.94033E+00 Friction velocity uk : 0.94033E+00 0.94033E+00 Dimensionless distance yplus : 0.91822E+00 0.91822E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.28525E+01 2 0.79707E-07 0.46092E-05 0.13828E-01 c Velocity[X] 0.46092E-05 c Velocity[Y] 0.32427E-32 c Velocity[Z] 0.19098E-63 c Pressure 0.21684E-18 0 0.10000E+01 -0.21684E-18 0.00000E+00 c k 0.15870E+00 5 0.47487E-08 0.15665E-06 0.26497E-01 c omega 0.12973E+03 1 0.49521E-08 0.21714E-04 0.14094E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.86343 18.647 13.285 16.598 v Velocity[Y] -1.3407e-16 1.6887e-17 -4.3902e-17 -3.5046e-17 v Velocity[Z] -3.0063e-32 4.793e-34 -4.9539e-33 -1.0784e-33 v ǁVelocityǁ 0.86343 18.647 13.285 16.598 v Pressure 0 0 0 0 v k 0.0010508 2.2861 1.534 1.418 v omega 6.7624 28194 1408.4 222.56 v TurbVisc 3.727e-08 0.12294 0.047523 0.083078 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.91822 0.45911 0.45911 INSTANT 0.110000000E+06 TIME STEP NUMBER 110000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94925E+00 0.94925E+00 Friction velocity uk : 0.94925E+00 0.94925E+00 Dimensionless distance yplus : 0.92692E+00 0.92692E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.29256E+01 2 0.66512E-07 0.33197E-05 0.11694E-01 c Velocity[X] 0.33197E-05 c Velocity[Y] 0.98758E-32 c Velocity[Z] 0.17739E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.16532E+00 5 0.39009E-08 0.11345E-06 0.22114E-01 c omega 0.12975E+03 1 0.42638E-08 0.15601E-04 0.12078E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.87988 18.852 13.442 16.784 v Velocity[Y] -2.0781e-16 1.168e-17 -7.1068e-17 -7.8913e-17 v Velocity[Z] 1.3381e-61 1.3878e-32 2.2844e-33 5.8154e-34 v ǁVelocityǁ 0.87988 18.852 13.442 16.784 v Pressure 0 0 0 0 v k 0.0011067 2.3378 1.5729 1.4548 v omega 6.8545 28194 1409.5 222.95 v TurbVisc 3.9254e-08 0.12499 0.048272 0.0844 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.92692 0.46346 0.46346 INSTANT 0.120000000E+06 TIME STEP NUMBER 120000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95676E+00 0.95676E+00 Friction velocity uk : 0.95676E+00 0.95676E+00 Dimensionless distance yplus : 0.93425E+00 0.93425E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.29873E+01 2 0.55743E-07 0.24011E-05 0.99124E-02 c Velocity[X] 0.24011E-05 c Velocity[Y] 0.16178E-31 c Velocity[Z] 0.15402E-65 c Pressure 0.21684E-18 0 0.10000E+01 -0.21684E-18 0.00000E+00 c k 0.17100E+00 5 0.32516E-08 0.83614E-07 0.18705E-01 c omega 0.12977E+03 1 0.36551E-08 0.11290E-04 0.10336E-03 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.89386 19.026 13.574 16.941 v Velocity[Y] -1.1779e-16 2.9875e-17 -3.8813e-17 -4.2363e-17 v Velocity[Z] -6.288e-33 3.1349e-33 2.3802e-34 1.5384e-34 v ǁVelocityǁ 0.89386 19.026 13.574 16.941 v Pressure 0 0 0 0 v k 0.0011556 2.3817 1.606 1.4862 v omega 6.9328 28194 1410.4 223.28 v TurbVisc 4.099e-08 0.12667 0.048895 0.085493 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.93425 0.46713 0.46713 INSTANT 0.130000000E+06 TIME STEP NUMBER 130000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96289E+00 0.96289E+00 Friction velocity uk : 0.96289E+00 0.96289E+00 Dimensionless distance yplus : 0.94024E+00 0.94024E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.30385E+01 1 0.18832E-06 0.11296E-05 0.67724E-02 c Velocity[X] 0.11296E-05 c Velocity[Y] 0.56030E-32 c Velocity[Z] 0.13175E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.17585E+00 5 0.24180E-08 0.50279E-07 0.14559E-01 c omega 0.12979E+03 1 0.26776E-08 0.55755E-05 0.73173E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.90535 19.166 13.682 17.068 v Velocity[Y] -9.6029e-17 1.3658e-16 -3.0569e-17 -1.9687e-17 v Velocity[Z] -1.5354e-32 2.3439e-33 -1.093e-33 -1.0975e-34 v ǁVelocityǁ 0.90535 19.166 13.682 17.068 v Pressure 0 0 0 0 v k 0.001197 2.418 1.6337 1.5126 v omega 6.9992 28194 1411.2 223.55 v TurbVisc 4.2455e-08 0.12807 0.04942 0.086412 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.94024 0.47012 0.47012 INSTANT 0.140000000E+06 TIME STEP NUMBER 140000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96735E+00 0.96735E+00 Friction velocity uk : 0.96735E+00 0.96735E+00 Dimensionless distance yplus : 0.94460E+00 0.94460E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.30767E+01 1 0.16420E-06 0.87258E-06 0.59462E-02 c Velocity[X] 0.87258E-06 c Velocity[Y] 0.96766E-32 c Velocity[Z] 0.53879E-67 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.17949E+00 4 0.50824E-08 0.30301E-07 0.11022E-01 c omega 0.12980E+03 1 0.21831E-08 0.41077E-05 0.62295E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.91377 19.268 13.76 17.16 v Velocity[Y] -9.8644e-17 2.9133e-16 -5.7733e-18 1.5034e-17 v Velocity[Z] 2.0686e-57 4.0577e-32 7.8084e-33 1.9589e-33 v ǁVelocityǁ 0.91377 19.268 13.76 17.16 v Pressure 0 0 0 0 v k 0.0012277 2.4443 1.6538 1.5318 v omega 7.0499 28194 1411.7 223.74 v TurbVisc 4.3546e-08 0.12915 0.049809 0.087102 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.9446 0.4723 0.4723 INSTANT 0.150000000E+06 TIME STEP NUMBER 150000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97121E+00 0.97121E+00 Friction velocity uk : 0.97121E+00 0.97121E+00 Dimensionless distance yplus : 0.94837E+00 0.94837E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.31088E+01 1 0.14388E-06 0.67774E-06 0.52346E-02 c Velocity[X] 0.67774E-06 c Velocity[Y] 0.10226E-31 c Velocity[Z] 0.70214E-66 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.18249E+00 4 0.43934E-08 0.23579E-07 0.96306E-02 c omega 0.12981E+03 1 0.19398E-08 0.31705E-05 0.55175E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.92106 19.357 13.829 17.241 v Velocity[Y] -9.2544e-17 3.4659e-16 1.5016e-17 6.8527e-17 v Velocity[Z] -2.7594e-32 3.9536e-34 -3.241e-33 -6.266e-34 v ǁVelocityǁ 0.92106 19.357 13.829 17.241 v Pressure 0 0 0 0 v k 0.0012548 2.4673 1.6711 1.548 v omega 7.0887 28194 1412.2 223.91 v TurbVisc 4.4506e-08 0.12998 0.050122 0.08765 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.94837 0.47418 0.47418 INSTANT 0.160000000E+06 TIME STEP NUMBER 160000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97459E+00 0.97459E+00 Friction velocity uk : 0.97459E+00 0.97459E+00 Dimensionless distance yplus : 0.95167E+00 0.95167E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.31370E+01 1 0.12608E-06 0.52702E-06 0.46089E-02 c Velocity[X] 0.52702E-06 c Velocity[Y] 0.45082E-32 c Velocity[Z] 0.13131E-63 c Pressure 0.33410E-51 0 0.10000E+01 -0.33410E-51 0.00000E+00 c k 0.18516E+00 4 0.38672E-08 0.18672E-07 0.85215E-02 c omega 0.12982E+03 1 0.17225E-08 0.24682E-05 0.48855E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.92749 19.436 13.889 17.312 v Velocity[Y] -9.2204e-17 2.1801e-16 8.6299e-18 4.7113e-17 v Velocity[Z] -3.567e-32 2.0482e-34 -5.0019e-33 -1.1491e-33 v ǁVelocityǁ 0.92749 19.436 13.889 17.312 v Pressure 0 0 0 0 v k 0.001279 2.4875 1.6863 1.5624 v omega 7.123 28194 1412.6 224.06 v TurbVisc 4.5364e-08 0.13071 0.050396 0.088128 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.95167 0.47584 0.47584 INSTANT 0.170000000E+06 TIME STEP NUMBER 170000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97757E+00 0.97757E+00 Friction velocity uk : 0.97757E+00 0.97757E+00 Dimensionless distance yplus : 0.95458E+00 0.95458E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.31620E+01 1 0.11059E-06 0.41016E-06 0.40601E-02 c Velocity[X] 0.41016E-06 c Velocity[Y] 0.27412E-32 c Velocity[Z] 0.51648E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.18753E+00 4 0.33911E-08 0.14653E-07 0.75075E-02 c omega 0.12983E+03 1 0.15227E-08 0.19224E-05 0.43185E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.93317 19.505 13.942 17.375 v Velocity[Y] -1.1646e-16 1.0558e-16 -1.005e-17 1.1152e-17 v Velocity[Z] -1.7391e-33 1.6255e-32 1.4393e-33 1.8146e-34 v ǁVelocityǁ 0.93317 19.505 13.942 17.375 v Pressure 0 0 0 0 v k 0.0013006 2.5054 1.6998 1.5751 v omega 7.1534 28194 1413 224.19 v TurbVisc 4.6129e-08 0.13135 0.050638 0.08855 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.95458 0.47729 0.47729 INSTANT 0.180000000E+06 TIME STEP NUMBER 180000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98020E+00 0.98020E+00 Friction velocity uk : 0.98020E+00 0.98020E+00 Dimensionless distance yplus : 0.95714E+00 0.95714E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.31841E+01 1 0.97107E-07 0.31947E-06 0.35788E-02 c Velocity[X] 0.31947E-06 c Velocity[Y] 0.63533E-32 c Velocity[Z] 0.13268E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.18963E+00 4 0.29728E-08 0.11473E-07 0.66095E-02 c omega 0.12984E+03 1 0.13454E-08 0.14979E-05 0.38168E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.93819 19.566 13.988 17.43 v Velocity[Y] -1.1633e-16 6.0439e-17 -3.2414e-17 -2.4152e-17 v Velocity[Z] -4.999e-33 1.6502e-32 3.3406e-34 -8.1051e-35 v ǁVelocityǁ 0.93819 19.566 13.988 17.43 v Pressure 0 0 0 0 v k 0.0013198 2.5212 1.7118 1.5863 v omega 7.1802 28194 1413.3 224.31 v TurbVisc 4.6812e-08 0.13191 0.050851 0.088921 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.95714 0.47857 0.47857 INSTANT 0.190000000E+06 TIME STEP NUMBER 190000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98251E+00 0.98251E+00 Friction velocity uk : 0.98251E+00 0.98251E+00 Dimensionless distance yplus : 0.95940E+00 0.95940E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32036E+01 1 0.85355E-07 0.24901E-06 0.31562E-02 c Velocity[X] 0.24901E-06 c Velocity[Y] 0.55271E-32 c Velocity[Z] 0.12886E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.19150E+00 4 0.26090E-08 0.89836E-08 0.58228E-02 c omega 0.12985E+03 1 0.11890E-08 0.11678E-05 0.33741E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.94262 19.62 14.029 17.478 v Velocity[Y] -1.7258e-16 4.3725e-17 -5.9224e-17 -5.9947e-17 v Velocity[Z] -2.8669e-32 4.3197e-35 -4.679e-33 -1.0838e-33 v ǁVelocityǁ 0.94262 19.62 14.029 17.478 v Pressure 0 0 0 0 v k 0.001337 2.5351 1.7223 1.5962 v omega 7.2038 28194 1413.6 224.41 v TurbVisc 4.742e-08 0.1324 0.051038 0.089248 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.9594 0.4797 0.4797 INSTANT 0.200000000E+06 TIME STEP NUMBER 200000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98454E+00 0.98454E+00 Friction velocity uk : 0.98454E+00 0.98454E+00 Dimensionless distance yplus : 0.96139E+00 0.96139E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32209E+01 1 0.75090E-07 0.19422E-06 0.27847E-02 c Velocity[X] 0.19422E-06 c Velocity[Y] 0.40197E-32 c Velocity[Z] 0.43268E-65 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.19316E+00 4 0.22923E-08 0.70357E-08 0.51330E-02 c omega 0.12985E+03 1 0.10511E-08 0.91105E-06 0.29833E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.94653 19.668 14.065 17.521 v Velocity[Y] -2.5443e-16 3.7865e-19 -6.3809e-17 -8.3942e-17 v Velocity[Z] -2.9984e-32 4.1965e-35 -3.9423e-33 -9.1756e-34 v ǁVelocityǁ 0.94653 19.668 14.065 17.521 v Pressure 0 0 0 0 v k 0.0013522 2.5474 1.7317 1.605 v omega 7.2246 28194 1413.9 224.5 v TurbVisc 4.7962e-08 0.13284 0.051203 0.089536 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.96139 0.48069 0.48069 INSTANT 0.210000000E+06 TIME STEP NUMBER 210000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98634E+00 0.98634E+00 Friction velocity uk : 0.98634E+00 0.98634E+00 Dimensionless distance yplus : 0.96314E+00 0.96314E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32361E+01 1 0.66108E-07 0.15157E-06 0.24579E-02 c Velocity[X] 0.15157E-06 c Velocity[Y] 0.95521E-32 c Velocity[Z] 0.62836E-66 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.19462E+00 4 0.20159E-08 0.55106E-08 0.45272E-02 c omega 0.12986E+03 1 0.92934E-09 0.71113E-06 0.26381E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.94999 19.709 14.097 17.559 v Velocity[Y] -1.4135e-16 3.2748e-17 -5.2047e-17 -6.3156e-17 v Velocity[Z] -1.6744e-32 2.8567e-35 -3.4801e-33 -8.7225e-34 v ǁVelocityǁ 0.94999 19.709 14.097 17.559 v Pressure 0 0 0 0 v k 0.0013658 2.5583 1.7399 1.6128 v omega 7.2429 28194 1414.1 224.58 v TurbVisc 4.8444e-08 0.13322 0.051349 0.08979 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.96314 0.48157 0.48157 INSTANT 0.220000000E+06 TIME STEP NUMBER 220000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98793E+00 0.98793E+00 Friction velocity uk : 0.98793E+00 0.98793E+00 Dimensionless distance yplus : 0.96469E+00 0.96469E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32496E+01 1 0.58239E-07 0.11834E-06 0.21702E-02 c Velocity[X] 0.11834E-06 c Velocity[Y] 0.77358E-32 c Velocity[Z] 0.12703E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.19592E+00 4 0.17742E-08 0.43163E-08 0.39947E-02 c omega 0.12986E+03 1 0.82179E-09 0.55534E-06 0.23332E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.95304 19.746 14.125 17.592 v Velocity[Y] -1.0484e-16 4.8637e-17 -3.8323e-17 -4.1191e-17 v Velocity[Z] -3.544e-32 1.7924e-35 -5.6257e-33 -1.3106e-33 v ǁVelocityǁ 0.95304 19.746 14.125 17.592 v Pressure 0 0 0 0 v k 0.0013779 2.5679 1.7472 1.6196 v omega 7.259 28194 1414.3 224.65 v TurbVisc 4.8872e-08 0.13356 0.051477 0.090014 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.96469 0.48235 0.48235 INSTANT 0.230000000E+06 TIME STEP NUMBER 230000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98933E+00 0.98933E+00 Friction velocity uk : 0.98933E+00 0.98933E+00 Dimensionless distance yplus : 0.96606E+00 0.96606E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32615E+01 1 0.51335E-07 0.92436E-07 0.19168E-02 c Velocity[X] 0.92436E-07 c Velocity[Y] 0.41963E-32 c Velocity[Z] 0.20538E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.19707E+00 4 0.15626E-08 0.33811E-08 0.35261E-02 c omega 0.12987E+03 1 0.72678E-09 0.43385E-06 0.20637E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.95575 19.779 14.15 17.621 v Velocity[Y] -1.1615e-16 9.8681e-17 -3.425e-17 -2.2134e-17 v Velocity[Z] -1.9346e-32 1.7924e-35 -3.8632e-33 -9.3328e-34 v ǁVelocityǁ 0.95575 19.779 14.15 17.621 v Pressure 0 0 0 0 v k 0.0013886 2.5764 1.7536 1.6257 v omega 7.2733 28194 1414.5 224.71 v TurbVisc 4.9253e-08 0.13386 0.051591 0.090211 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.96606 0.48303 0.48303 INSTANT 0.240000000E+06 TIME STEP NUMBER 240000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99056E+00 0.99056E+00 Friction velocity uk : 0.99056E+00 0.99056E+00 Dimensionless distance yplus : 0.96726E+00 0.96726E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32721E+01 1 0.45273E-07 0.72230E-07 0.16934E-02 c Velocity[X] 0.72230E-07 c Velocity[Y] 0.18168E-31 c Velocity[Z] 0.16734E-65 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.19809E+00 4 0.13770E-08 0.26485E-08 0.31136E-02 c omega 0.12987E+03 1 0.64282E-09 0.33906E-06 0.18255E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.95814 19.808 14.172 17.647 v Velocity[Y] -8.9566e-17 1.1512e-16 -2.0567e-17 -1.5564e-17 v Velocity[Z] -1.2458e-32 1.0784e-35 -2.0131e-33 -4.7415e-34 v ǁVelocityǁ 0.95814 19.808 14.172 17.647 v Pressure 0 0 0 0 v k 0.0013982 2.584 1.7593 1.631 v omega 7.2858 28194 1414.6 224.77 v TurbVisc 4.9591e-08 0.13412 0.051691 0.090385 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.96726 0.48363 0.48363 INSTANT 0.250000000E+06 TIME STEP NUMBER 250000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99165E+00 0.99165E+00 Friction velocity uk : 0.99165E+00 0.99165E+00 Dimensionless distance yplus : 0.96833E+00 0.96833E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 250000, Physical time 0.25000E+06 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 250000: 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 0.32813E+01 1 0.39960E-07 0.56484E-07 0.14968E-02 c Velocity[X] 0.56484E-07 c Velocity[Y] 0.29883E-32 c Velocity[Z] 0.12623E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.19899E+00 3 0.45474E-08 0.20731E-08 0.27482E-02 c omega 0.12987E+03 1 0.56929E-09 0.26502E-06 0.16160E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.96025 19.833 14.191 17.67 v Velocity[Y] -9.3028e-17 1.8187e-16 -9.3892e-18 1.0996e-17 v Velocity[Z] -1.1915e-33 4.714e-33 4.343e-34 2.7775e-35 v ǁVelocityǁ 0.96025 19.833 14.191 17.67 v Pressure 0 0 0 0 v k 0.0014066 2.5906 1.7644 1.6357 v omega 7.2969 28194 1414.8 224.82 v TurbVisc 4.9891e-08 0.13435 0.051778 0.090538 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.96833 0.48416 0.48416 INSTANT 0.260000000E+06 TIME STEP NUMBER 260000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99262E+00 0.99262E+00 Friction velocity uk : 0.99262E+00 0.99262E+00 Dimensionless distance yplus : 0.96927E+00 0.96927E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32896E+01 1 0.35264E-07 0.44163E-07 0.13228E-02 c Velocity[X] 0.44163E-07 c Velocity[Y] 0.51862E-32 c Velocity[Z] 0.27023E-65 c Pressure 0.67763E-20 0 0.10000E+01 -0.67763E-20 0.00000E+00 c k 0.19979E+00 3 0.40237E-08 0.16298E-08 0.24334E-02 c omega 0.12988E+03 1 0.50343E-09 0.20740E-06 0.14294E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.96212 19.856 14.209 17.691 v Velocity[Y] -9.3004e-17 2.926e-16 1.031e-17 5.425e-17 v Velocity[Z] -1.4961e-32 1.0751e-35 -3.5289e-33 -9.6579e-34 v ǁVelocityǁ 0.96212 19.856 14.209 17.691 v Pressure 0 0 0 0 v k 0.0014141 2.5965 1.7688 1.6399 v omega 7.3067 28194 1414.9 224.86 v TurbVisc 5.0158e-08 0.13456 0.051856 0.090673 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.96927 0.48464 0.48464 INSTANT 0.270000000E+06 TIME STEP NUMBER 270000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99347E+00 0.99347E+00 Friction velocity uk : 0.99347E+00 0.99347E+00 Dimensionless distance yplus : 0.97010E+00 0.97010E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32969E+01 1 0.31133E-07 0.34536E-07 0.11693E-02 c Velocity[X] 0.34536E-07 c Velocity[Y] 0.11832E-31 c Velocity[Z] 0.12243E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20050E+00 3 0.35494E-08 0.12758E-08 0.21494E-02 c omega 0.12988E+03 1 0.44510E-09 0.16222E-06 0.12644E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.96377 19.875 14.224 17.708 v Velocity[Y] -1.2925e-16 3.335e-16 2.1552e-17 7.032e-17 v Velocity[Z] -2.2911e-32 1.0751e-35 -2.8735e-33 -6.5752e-34 v ǁVelocityǁ 0.96377 19.875 14.224 17.708 v Pressure 0 0 0 0 v k 0.0014208 2.6017 1.7728 1.6436 v omega 7.3153 28194 1415 224.9 v TurbVisc 5.0394e-08 0.13474 0.051925 0.090794 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.9701 0.48505 0.48505 INSTANT 0.280000000E+06 TIME STEP NUMBER 280000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99422E+00 0.99422E+00 Friction velocity uk : 0.99422E+00 0.99422E+00 Dimensionless distance yplus : 0.97084E+00 0.97084E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33033E+01 1 0.27496E-07 0.27015E-07 0.10338E-02 c Velocity[X] 0.27015E-07 c Velocity[Y] 0.92101E-32 c Velocity[Z] 0.99431E-66 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20113E+00 3 0.31326E-08 0.99908E-09 0.18993E-02 c omega 0.12988E+03 1 0.39373E-09 0.12689E-06 0.11186E-04 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.96523 19.893 14.237 17.724 v Velocity[Y] -1.2041e-16 3.8067e-16 2.6107e-17 9.0309e-17 v Velocity[Z] -2.6245e-32 1.0747e-35 -4.1767e-33 -9.788e-34 v ǁVelocityǁ 0.96523 19.893 14.237 17.724 v Pressure 0 0 0 0 v k 0.0014267 2.6063 1.7763 1.6469 v omega 7.323 28194 1415.1 224.93 v TurbVisc 5.0604e-08 0.1349 0.051986 0.0909 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97084 0.48542 0.48542 INSTANT 0.290000000E+06 TIME STEP NUMBER 290000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99489E+00 0.99489E+00 Friction velocity uk : 0.99489E+00 0.99489E+00 Dimensionless distance yplus : 0.97149E+00 0.97149E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33090E+01 1 0.24290E-07 0.21135E-07 0.91413E-03 c Velocity[X] 0.21135E-07 c Velocity[Y] 0.47213E-32 c Velocity[Z] 0.40703E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20168E+00 3 0.27662E-08 0.78266E-09 0.16790E-02 c omega 0.12988E+03 1 0.34836E-09 0.99284E-07 0.98981E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.96653 19.908 14.249 17.738 v Velocity[Y] -1.072e-16 4.5091e-16 3.5382e-17 1.1013e-16 v Velocity[Z] -1.4846e-34 2.1103e-32 3.6948e-33 9.5593e-34 v ǁVelocityǁ 0.96653 19.908 14.249 17.738 v Pressure 0 0 0 0 v k 0.001432 2.6104 1.7793 1.6498 v omega 7.3298 28194 1415.2 224.96 v TurbVisc 5.079e-08 0.13504 0.05204 0.090994 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97149 0.48575 0.48575 INSTANT 0.300000000E+06 TIME STEP NUMBER 300000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99548E+00 0.99548E+00 Friction velocity uk : 0.99548E+00 0.99548E+00 Dimensionless distance yplus : 0.97207E+00 0.97207E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33141E+01 1 0.21463E-07 0.16538E-07 0.80841E-03 c Velocity[X] 0.16538E-07 c Velocity[Y] 0.69263E-32 c Velocity[Z] 0.12551E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20218E+00 3 0.24434E-08 0.61316E-09 0.14844E-02 c omega 0.12989E+03 1 0.30825E-09 0.77696E-07 0.87587E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.96767 19.922 14.259 17.751 v Velocity[Y] -1.0465e-16 4.3639e-16 3.6786e-17 1.1882e-16 v Velocity[Z] -1.4632e-34 2.1536e-32 5.4415e-33 1.4305e-33 v ǁVelocityǁ 0.96767 19.922 14.259 17.751 v Pressure 0 0 0 0 v k 0.0014366 2.614 1.7821 1.6524 v omega 7.3357 28194 1415.3 224.99 v TurbVisc 5.0955e-08 0.13517 0.052088 0.091077 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97207 0.48603 0.48603 INSTANT 0.310000000E+06 TIME STEP NUMBER 310000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99600E+00 0.99600E+00 Friction velocity uk : 0.99600E+00 0.99600E+00 Dimensionless distance yplus : 0.97258E+00 0.97258E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33186E+01 1 0.18969E-07 0.12943E-07 0.71499E-03 c Velocity[X] 0.12943E-07 c Velocity[Y] 0.58601E-32 c Velocity[Z] 0.12749E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20261E+00 3 0.21588E-08 0.48037E-09 0.13126E-02 c omega 0.12989E+03 1 0.27276E-09 0.60810E-07 0.77507E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.96869 19.934 14.269 17.762 v Velocity[Y] -1.2035e-16 4.4833e-16 4.1977e-17 1.2457e-16 v Velocity[Z] -1.4387e-34 1.9664e-32 3.8135e-33 1.0612e-33 v ǁVelocityǁ 0.96869 19.934 14.269 17.762 v Pressure 0 0 0 0 v k 0.0014407 2.6172 1.7845 1.6547 v omega 7.341 28194 1415.3 225.01 v TurbVisc 5.1101e-08 0.13528 0.05213 0.09115 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97258 0.48629 0.48629 INSTANT 0.320000000E+06 TIME STEP NUMBER 320000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99646E+00 0.99646E+00 Friction velocity uk : 0.99646E+00 0.99646E+00 Dimensionless distance yplus : 0.97302E+00 0.97302E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33225E+01 1 0.16768E-07 0.10131E-07 0.63243E-03 c Velocity[X] 0.10131E-07 c Velocity[Y] 0.84069E-32 c Velocity[Z] 0.12856E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20300E+00 3 0.19078E-08 0.37635E-09 0.11608E-02 c omega 0.12989E+03 1 0.24137E-09 0.47601E-07 0.68590E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.96958 19.945 14.277 17.771 v Velocity[Y] -8.8421e-17 4.4916e-16 4.4713e-17 1.2798e-16 v Velocity[Z] -6.1982e-33 7.7267e-33 1.3782e-33 5.5422e-34 v ǁVelocityǁ 0.96958 19.945 14.277 17.771 v Pressure 0 0 0 0 v k 0.0014444 2.62 1.7866 1.6567 v omega 7.3457 28194 1415.4 225.03 v TurbVisc 5.1231e-08 0.13538 0.052167 0.091215 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97302 0.48651 0.48651 INSTANT 0.330000000E+06 TIME STEP NUMBER 330000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99687E+00 0.99687E+00 Friction velocity uk : 0.99687E+00 0.99687E+00 Dimensionless distance yplus : 0.97342E+00 0.97342E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33260E+01 1 0.14824E-07 0.79309E-08 0.55945E-03 c Velocity[X] 0.79309E-08 c Velocity[Y] 0.86109E-32 c Velocity[Z] 0.12558E-63 c Pressure 0.66819E-51 0 0.10000E+01 -0.66819E-51 0.00000E+00 c k 0.20334E+00 3 0.16863E-08 0.29485E-09 0.10267E-02 c omega 0.12989E+03 1 0.21360E-09 0.37265E-07 0.60701E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97037 19.954 14.284 17.78 v Velocity[Y] -8.8806e-17 4.6456e-16 5.4124e-17 1.3582e-16 v Velocity[Z] -4.1747e-35 3.107e-32 6.7099e-33 1.7339e-33 v ǁVelocityǁ 0.97037 19.954 14.284 17.78 v Pressure 0 0 0 0 v k 0.0014476 2.6225 1.7885 1.6584 v omega 7.3498 28194 1415.4 225.05 v TurbVisc 5.1346e-08 0.13547 0.0522 0.091273 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97342 0.48671 0.48671 INSTANT 0.340000000E+06 TIME STEP NUMBER 340000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99723E+00 0.99723E+00 Friction velocity uk : 0.99723E+00 0.99723E+00 Dimensionless distance yplus : 0.97377E+00 0.97377E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33291E+01 1 0.13108E-07 0.62091E-08 0.49493E-03 c Velocity[X] 0.62091E-08 c Velocity[Y] 0.51627E-32 c Velocity[Z] 0.12518E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20364E+00 3 0.14907E-08 0.23101E-09 0.90816E-03 c omega 0.12989E+03 1 0.18903E-09 0.29176E-07 0.53720E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97108 19.963 14.29 17.787 v Velocity[Y] -8.8609e-17 4.133e-16 4.2091e-17 1.2043e-16 v Velocity[Z] -4.174e-35 2.4911e-32 4.4397e-33 1.1364e-33 v ǁVelocityǁ 0.97108 19.963 14.29 17.787 v Pressure 0 0 0 0 v k 0.0014505 2.6247 1.7902 1.66 v omega 7.3534 28194 1415.5 225.06 v TurbVisc 5.1448e-08 0.13554 0.052229 0.091324 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97377 0.48689 0.48689 INSTANT 0.350000000E+06 TIME STEP NUMBER 350000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99755E+00 0.99755E+00 Friction velocity uk : 0.99755E+00 0.99755E+00 Dimensionless distance yplus : 0.97409E+00 0.97409E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33319E+01 1 0.11592E-07 0.48616E-08 0.43788E-03 c Velocity[X] 0.48616E-08 c Velocity[Y] 0.11861E-31 c Velocity[Z] 0.29173E-65 c Pressure 0.41762E-52 0 0.10000E+01 -0.41762E-52 0.00000E+00 c k 0.20391E+00 3 0.13181E-08 0.18099E-09 0.80337E-03 c omega 0.12989E+03 1 0.16729E-09 0.22845E-07 0.47543E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.9717 19.97 14.296 17.794 v Velocity[Y] -9.2822e-17 4.3128e-16 4.3407e-17 1.2656e-16 v Velocity[Z] -4.0985e-35 1.3287e-32 3.4409e-33 1.0827e-33 v ǁVelocityǁ 0.9717 19.97 14.296 17.794 v Pressure 0 0 0 0 v k 0.001453 2.6267 1.7917 1.6614 v omega 7.3567 28194 1415.5 225.08 v TurbVisc 5.1538e-08 0.13561 0.052255 0.091368 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97409 0.48704 0.48704 INSTANT 0.360000000E+06 TIME STEP NUMBER 360000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99783E+00 0.99783E+00 Friction velocity uk : 0.99783E+00 0.99783E+00 Dimensionless distance yplus : 0.97436E+00 0.97436E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33343E+01 1 0.10270E-07 0.38130E-08 0.38789E-03 c Velocity[X] 0.38130E-08 c Velocity[Y] 0.11388E-31 c Velocity[Z] 0.13304E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20414E+00 2 0.47447E-08 0.13881E-09 0.70118E-03 c omega 0.12989E+03 1 0.14850E-09 0.17834E-07 0.42171E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97224 19.977 14.301 17.8 v Velocity[Y] -9.8366e-17 3.7662e-16 3.8325e-17 1.1225e-16 v Velocity[Z] -4.051e-35 1.9413e-32 3.894e-33 1.0917e-33 v ǁVelocityǁ 0.97224 19.977 14.301 17.8 v Pressure 0 0 0 0 v k 0.0014553 2.6284 1.793 1.6626 v omega 7.3595 28194 1415.6 225.09 v TurbVisc 5.1617e-08 0.13567 0.052277 0.091407 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97436 0.48718 0.48718 INSTANT 0.370000000E+06 TIME STEP NUMBER 370000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99808E+00 0.99808E+00 Friction velocity uk : 0.99808E+00 0.99808E+00 Dimensionless distance yplus : 0.97460E+00 0.97460E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33364E+01 1 0.90787E-08 0.29865E-08 0.34314E-03 c Velocity[X] 0.29865E-08 c Velocity[Y] 0.14117E-31 c Velocity[Z] 0.48900E-63 c Pressure 0.83524E-52 0 0.10000E+01 -0.83524E-52 0.00000E+00 c k 0.20435E+00 2 0.43007E-08 0.11223E-09 0.63224E-03 c omega 0.12989E+03 1 0.13162E-09 0.14038E-07 0.37328E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97273 19.983 14.306 17.805 v Velocity[Y] -9.1402e-17 3.8604e-16 3.7466e-17 1.1436e-16 v Velocity[Z] -9.4681e-33 6.5064e-33 1.0924e-33 4.689e-34 v ǁVelocityǁ 0.97273 19.983 14.306 17.805 v Pressure 0 0 0 0 v k 0.0014573 2.6299 1.7941 1.6637 v omega 7.362 28194 1415.6 225.1 v TurbVisc 5.1688e-08 0.13572 0.052297 0.091441 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.9746 0.4873 0.4873 INSTANT 0.380000000E+06 TIME STEP NUMBER 380000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99830E+00 0.99830E+00 Friction velocity uk : 0.99830E+00 0.99830E+00 Dimensionless distance yplus : 0.97482E+00 0.97482E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33383E+01 1 0.80269E-08 0.23382E-08 0.30355E-03 c Velocity[X] 0.23382E-08 c Velocity[Y] 0.11235E-31 c Velocity[Z] 0.12664E-63 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20454E+00 2 0.38059E-08 0.87854E-10 0.55928E-03 c omega 0.12989E+03 1 0.11612E-09 0.11000E-07 0.32990E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97316 19.988 14.309 17.81 v Velocity[Y] -9.5969e-17 3.9196e-16 3.2251e-17 1.091e-16 v Velocity[Z] -4.0513e-35 1.8751e-32 3.953e-33 1.1007e-33 v ǁVelocityǁ 0.97316 19.988 14.309 17.81 v Pressure 0 0 0 0 v k 0.001459 2.6313 1.7952 1.6647 v omega 7.3643 28194 1415.6 225.11 v TurbVisc 5.1751e-08 0.13577 0.052315 0.091473 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97482 0.48741 0.48741 INSTANT 0.390000000E+06 TIME STEP NUMBER 390000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99850E+00 0.99850E+00 Friction velocity uk : 0.99850E+00 0.99850E+00 Dimensionless distance yplus : 0.97501E+00 0.97501E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33400E+01 1 0.70997E-08 0.18308E-08 0.26857E-03 c Velocity[X] 0.18308E-08 c Velocity[Y] 0.46264E-32 c Velocity[Z] 0.12689E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20471E+00 2 0.33613E-08 0.68666E-10 0.49418E-03 c omega 0.12989E+03 1 0.10264E-09 0.86112E-08 0.29179E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97354 19.992 14.313 17.814 v Velocity[Y] -8.8864e-17 3.2381e-16 3.1267e-17 9.2164e-17 v Velocity[Z] -4.0509e-35 2.7041e-32 6.0846e-33 1.6745e-33 v ǁVelocityǁ 0.97354 19.992 14.313 17.814 v Pressure 0 0 0 0 v k 0.0014606 2.6325 1.7961 1.6655 v omega 7.3663 28194 1415.7 225.12 v TurbVisc 5.1806e-08 0.13581 0.052331 0.0915 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97501 0.48751 0.48751 INSTANT 0.400000000E+06 TIME STEP NUMBER 400000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99867E+00 0.99867E+00 Friction velocity uk : 0.99867E+00 0.99867E+00 Dimensionless distance yplus : 0.97518E+00 0.97518E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33415E+01 1 0.62804E-08 0.14336E-08 0.23763E-03 c Velocity[X] 0.14336E-08 c Velocity[Y] 0.15481E-32 c Velocity[Z] 0.12541E-63 c Pressure 0.33410E-51 0 0.10000E+01 -0.33410E-51 0.00000E+00 c k 0.20485E+00 2 0.29720E-08 0.53760E-10 0.43710E-03 c omega 0.12989E+03 1 0.90813E-10 0.67424E-08 0.25821E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97388 19.996 14.316 17.818 v Velocity[Y] -8.8609e-17 3.1065e-16 3.1882e-17 9.5046e-17 v Velocity[Z] -4.0423e-35 3.95e-32 6.9831e-33 1.7597e-33 v ǁVelocityǁ 0.97388 19.996 14.316 17.818 v Pressure 0 0 0 0 v k 0.001462 2.6336 1.7969 1.6663 v omega 7.368 28194 1415.7 225.13 v TurbVisc 5.1855e-08 0.13585 0.052345 0.091525 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97518 0.48759 0.48759 INSTANT 0.410000000E+06 TIME STEP NUMBER 410000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99882E+00 0.99882E+00 Friction velocity uk : 0.99882E+00 0.99882E+00 Dimensionless distance yplus : 0.97533E+00 0.97533E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33428E+01 1 0.55561E-08 0.11226E-08 0.21027E-03 c Velocity[X] 0.11226E-08 c Velocity[Y] 0.17088E-31 c Velocity[Z] 0.62151E-66 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20498E+00 2 0.26289E-08 0.42110E-10 0.38674E-03 c omega 0.12990E+03 1 0.80368E-10 0.52798E-08 0.22852E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97418 20 14.319 17.821 v Velocity[Y] -1.1145e-16 3.2681e-16 3.9809e-17 1.0096e-16 v Velocity[Z] 2.6038e-56 1.963e-32 4.5992e-33 1.3298e-33 v ǁVelocityǁ 0.97418 20 14.319 17.821 v Pressure 0 0 0 0 v k 0.0014632 2.6345 1.7976 1.667 v omega 7.3696 28194 1415.7 225.13 v TurbVisc 5.1899e-08 0.13588 0.052357 0.091547 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97533 0.48766 0.48766 INSTANT 0.420000000E+06 TIME STEP NUMBER 420000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99896E+00 0.99896E+00 Friction velocity uk : 0.99896E+00 0.99896E+00 Dimensionless distance yplus : 0.97546E+00 0.97546E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33440E+01 1 0.49155E-08 0.87909E-09 0.18606E-03 c Velocity[X] 0.87909E-09 c Velocity[Y] 0.55017E-32 c Velocity[Z] 0.30106E-65 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20510E+00 2 0.23257E-08 0.32986E-10 0.34220E-03 c omega 0.12990E+03 1 0.71126E-10 0.41347E-08 0.20224E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97444 20.003 14.321 17.824 v Velocity[Y] -1.027e-16 3.695e-16 4.9393e-17 1.1779e-16 v Velocity[Z] 2.6051e-56 2.5292e-32 4.0384e-33 1.1177e-33 v ǁVelocityǁ 0.97444 20.003 14.321 17.824 v Pressure 0 0 0 0 v k 0.0014643 2.6353 1.7982 1.6676 v omega 7.3709 28194 1415.7 225.14 v TurbVisc 5.1938e-08 0.13591 0.052368 0.091566 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97546 0.48773 0.48773 INSTANT 0.430000000E+06 TIME STEP NUMBER 430000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99908E+00 0.99908E+00 Friction velocity uk : 0.99908E+00 0.99908E+00 Dimensionless distance yplus : 0.97558E+00 0.97558E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33450E+01 1 0.43490E-08 0.68844E-09 0.16465E-03 c Velocity[X] 0.68844E-09 c Velocity[Y] 0.67513E-32 c Velocity[Z] 0.49956E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20520E+00 2 0.20575E-08 0.25839E-10 0.30280E-03 c omega 0.12990E+03 1 0.62946E-10 0.32380E-08 0.17898E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97468 20.006 14.323 17.826 v Velocity[Y] -8.8258e-17 4.1518e-16 4.9626e-17 1.2279e-16 v Velocity[Z] -2.344e-34 7.3938e-33 1.6738e-33 6.2189e-34 v ǁVelocityǁ 0.97468 20.006 14.323 17.826 v Pressure 0 0 0 0 v k 0.0014653 2.6361 1.7988 1.6681 v omega 7.3722 28194 1415.7 225.14 v TurbVisc 5.1972e-08 0.13593 0.052378 0.091583 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97558 0.48779 0.48779 INSTANT 0.440000000E+06 TIME STEP NUMBER 440000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99918E+00 0.99918E+00 Friction velocity uk : 0.99918E+00 0.99918E+00 Dimensionless distance yplus : 0.97568E+00 0.97568E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33459E+01 1 0.38479E-08 0.53916E-09 0.14570E-03 c Velocity[X] 0.53916E-09 c Velocity[Y] 0.56226E-32 c Velocity[Z] 0.12600E-63 c Pressure 0.67763E-20 0 0.10000E+01 -0.67763E-20 0.00000E+00 c k 0.20529E+00 2 0.18203E-08 0.20240E-10 0.26794E-03 c omega 0.12990E+03 1 0.55708E-10 0.25359E-08 0.15840E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97489 20.008 14.325 17.828 v Velocity[Y] -8.6825e-17 3.2584e-16 5.2156e-17 1.1366e-16 v Velocity[Z] 2.6052e-56 9.1178e-33 2.6381e-33 8.8942e-34 v ǁVelocityǁ 0.97489 20.008 14.325 17.828 v Pressure 0 0 0 0 v k 0.0014661 2.6367 1.7993 1.6685 v omega 7.3732 28194 1415.7 225.15 v TurbVisc 5.2002e-08 0.13596 0.052387 0.091598 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97568 0.48784 0.48784 INSTANT 0.450000000E+06 TIME STEP NUMBER 450000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99928E+00 0.99928E+00 Friction velocity uk : 0.99928E+00 0.99928E+00 Dimensionless distance yplus : 0.97577E+00 0.97577E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33467E+01 1 0.34047E-08 0.42225E-09 0.12893E-03 c Velocity[X] 0.42225E-09 c Velocity[Y] 0.47706E-32 c Velocity[Z] 0.13408E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20537E+00 2 0.16106E-08 0.15854E-10 0.23710E-03 c omega 0.12990E+03 1 0.49302E-10 0.19861E-08 0.14019E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97507 20.01 14.327 17.83 v Velocity[Y] -8.659e-17 4.2221e-16 5.6418e-17 1.2797e-16 v Velocity[Z] 2.6052e-56 3.4229e-32 5.4473e-33 1.4698e-33 v ǁVelocityǁ 0.97507 20.01 14.327 17.83 v Pressure 0 0 0 0 v k 0.0014669 2.6373 1.7997 1.669 v omega 7.3742 28194 1415.8 225.15 v TurbVisc 5.2029e-08 0.13598 0.052394 0.091611 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97577 0.48789 0.48789 INSTANT 0.460000000E+06 TIME STEP NUMBER 460000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99936E+00 0.99936E+00 Friction velocity uk : 0.99936E+00 0.99936E+00 Dimensionless distance yplus : 0.97586E+00 0.97586E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33475E+01 1 0.30126E-08 0.33071E-09 0.11410E-03 c Velocity[X] 0.33071E-09 c Velocity[Y] 0.39725E-32 c Velocity[Z] 0.32316E-65 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20544E+00 2 0.14250E-08 0.12419E-10 0.20982E-03 c omega 0.12990E+03 1 0.43633E-10 0.15555E-08 0.12407E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97523 20.012 14.328 17.832 v Velocity[Y] -8.65e-17 3.8333e-16 5.8021e-17 1.2489e-16 v Velocity[Z] 2.6052e-56 1.6487e-32 4.1257e-33 1.2861e-33 v ǁVelocityǁ 0.97523 20.012 14.328 17.832 v Pressure 0 0 0 0 v k 0.0014676 2.6378 1.8001 1.6693 v omega 7.375 28194 1415.8 225.16 v TurbVisc 5.2053e-08 0.13599 0.052401 0.091623 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97586 0.48793 0.48793 INSTANT 0.470000000E+06 TIME STEP NUMBER 470000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99943E+00 0.99943E+00 Friction velocity uk : 0.99943E+00 0.99943E+00 Dimensionless distance yplus : 0.97593E+00 0.97593E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33481E+01 1 0.26658E-08 0.25901E-09 0.10097E-03 c Velocity[X] 0.25901E-09 c Velocity[Y] 0.80047E-32 c Velocity[Z] 0.12886E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20550E+00 2 0.12609E-08 0.97283E-11 0.18567E-03 c omega 0.12990E+03 1 0.38616E-10 0.12183E-08 0.10981E-05 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97538 20.014 14.33 17.834 v Velocity[Y] -8.6276e-17 4.1614e-16 6.7793e-17 1.4242e-16 v Velocity[Z] 2.6052e-56 3.6912e-32 5.5454e-33 1.3947e-33 v ǁVelocityǁ 0.97538 20.014 14.33 17.834 v Pressure 0 0 0 0 v k 0.0014682 2.6383 1.8005 1.6696 v omega 7.3758 28194 1415.8 225.16 v TurbVisc 5.2074e-08 0.13601 0.052407 0.091633 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97593 0.48796 0.48796 INSTANT 0.480000000E+06 TIME STEP NUMBER 480000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99950E+00 0.99950E+00 Friction velocity uk : 0.99950E+00 0.99950E+00 Dimensionless distance yplus : 0.97599E+00 0.97599E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33486E+01 1 0.23717E-08 0.20404E-09 0.89715E-04 c Velocity[X] 0.20404E-09 c Velocity[Y] 0.73718E-32 c Velocity[Z] 0.12794E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20555E+00 1 0.49662E-08 0.62948E-11 0.14819E-03 c omega 0.12990E+03 1 0.34491E-10 0.94993E-09 0.98181E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.9755 20.016 14.331 17.835 v Velocity[Y] -8.6587e-17 3.8783e-16 6.2349e-17 1.2913e-16 v Velocity[Z] 2.6052e-56 2.6608e-32 4.7407e-33 1.2899e-33 v ǁVelocityǁ 0.9755 20.016 14.331 17.835 v Pressure 0 0 0 0 v k 0.0014687 2.6386 1.8008 1.6699 v omega 7.3764 28194 1415.8 225.16 v TurbVisc 5.2092e-08 0.13602 0.052412 0.091641 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97599 0.48799 0.48799 INSTANT 0.490000000E+06 TIME STEP NUMBER 490000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99955E+00 0.99955E+00 Friction velocity uk : 0.99955E+00 0.99955E+00 Dimensionless distance yplus : 0.97605E+00 0.97605E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33491E+01 1 0.21010E-08 0.16032E-09 0.79497E-04 c Velocity[X] 0.16032E-09 c Velocity[Y] 0.55594E-32 c Velocity[Z] 0.12491E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20560E+00 1 0.48784E-08 0.59482E-11 0.14473E-03 c omega 0.12990E+03 1 0.30822E-10 0.74972E-09 0.86959E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97561 20.017 14.332 17.836 v Velocity[Y] -8.6089e-17 4.071e-16 6.5857e-17 1.3501e-16 v Velocity[Z] 2.6052e-56 5.5179e-33 2.0451e-33 7.3578e-34 v ǁVelocityǁ 0.97561 20.017 14.332 17.836 v Pressure 0 0 0 0 v k 0.0014691 2.639 1.801 1.6702 v omega 7.377 28194 1415.8 225.17 v TurbVisc 5.2108e-08 0.13603 0.052416 0.091649 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97605 0.48802 0.48802 INSTANT 0.500000000E+06 TIME STEP NUMBER 500000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99961E+00 0.99961E+00 Friction velocity uk : 0.99961E+00 0.99961E+00 Dimensionless distance yplus : 0.97610E+00 0.97610E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 500000, Physical time 0.50000E+06 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 500000: 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 0.33495E+01 1 0.18552E-08 0.12550E-09 0.70279E-04 c Velocity[X] 0.12550E-09 c Velocity[Y] 0.10689E-31 c Velocity[Z] 0.51520E-63 c Pressure 0.12529E-51 0 0.10000E+01 -0.12529E-51 0.00000E+00 c k 0.20564E+00 1 0.44783E-08 0.48736E-11 0.13164E-03 c omega 0.12990E+03 1 0.27078E-10 0.59218E-09 0.76634E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97571 20.018 14.333 17.837 v Velocity[Y] -1.1121e-16 4.3142e-16 6.6045e-17 1.4179e-16 v Velocity[Z] -5.0715e-33 1.3564e-32 3.1625e-33 1.0739e-33 v ǁVelocityǁ 0.97571 20.018 14.333 17.837 v Pressure 0 0 0 0 v k 0.0014695 2.6393 1.8013 1.6704 v omega 7.3775 28194 1415.8 225.17 v TurbVisc 5.2123e-08 0.13604 0.05242 0.091656 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.9761 0.48805 0.48805 INSTANT 0.510000000E+06 TIME STEP NUMBER 510000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99965E+00 0.99965E+00 Friction velocity uk : 0.99965E+00 0.99965E+00 Dimensionless distance yplus : 0.97614E+00 0.97614E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33499E+01 1 0.16392E-08 0.98164E-10 0.62134E-04 c Velocity[X] 0.98164E-10 c Velocity[Y] 0.80397E-32 c Velocity[Z] 0.71285E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20568E+00 1 0.39695E-08 0.38123E-11 0.11648E-03 c omega 0.12990E+03 1 0.23756E-10 0.46382E-09 0.67543E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.9758 20.019 14.333 17.838 v Velocity[Y] -8.6276e-17 4.0105e-16 6.4374e-17 1.3886e-16 v Velocity[Z] -6.1896e-33 9.5905e-33 2.178e-33 8.2371e-34 v ǁVelocityǁ 0.9758 20.019 14.333 17.838 v Pressure 0 0 0 0 v k 0.0014699 2.6396 1.8015 1.6706 v omega 7.378 28194 1415.8 225.17 v TurbVisc 5.2136e-08 0.13605 0.052424 0.091662 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97614 0.48807 0.48807 INSTANT 0.520000000E+06 TIME STEP NUMBER 520000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99969E+00 0.99969E+00 Friction velocity uk : 0.99969E+00 0.99969E+00 Dimensionless distance yplus : 0.97618E+00 0.97618E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33503E+01 1 0.14494E-08 0.76778E-10 0.54947E-04 c Velocity[X] 0.76778E-10 c Velocity[Y] 0.17490E-31 c Velocity[Z] 0.69109E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20571E+00 1 0.35022E-08 0.29707E-11 0.10279E-03 c omega 0.12990E+03 1 0.20947E-10 0.36268E-09 0.59661E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97588 20.02 14.334 17.839 v Velocity[Y] -8.9464e-17 4.2738e-16 6.3488e-17 1.4068e-16 v Velocity[Z] -2.1625e-33 1.3692e-32 3.1519e-33 1.0363e-33 v ǁVelocityǁ 0.97588 20.02 14.334 17.839 v Pressure 0 0 0 0 v k 0.0014702 2.6398 1.8017 1.6708 v omega 7.3784 28194 1415.8 225.17 v TurbVisc 5.2147e-08 0.13606 0.052427 0.091668 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97618 0.48809 0.48809 INSTANT 0.530000000E+06 TIME STEP NUMBER 530000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99973E+00 0.99973E+00 Friction velocity uk : 0.99973E+00 0.99973E+00 Dimensionless distance yplus : 0.97621E+00 0.97621E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33506E+01 1 0.12818E-08 0.60055E-10 0.48595E-04 c Velocity[X] 0.60055E-10 c Velocity[Y] 0.10011E-31 c Velocity[Z] 0.13854E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20574E+00 1 0.30938E-08 0.23205E-11 0.90829E-04 c omega 0.12990E+03 1 0.18515E-10 0.28362E-09 0.52754E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97595 20.021 14.335 17.84 v Velocity[Y] -8.6405e-17 3.9083e-16 5.9967e-17 1.3036e-16 v Velocity[Z] 2.6052e-56 3.2172e-32 5e-33 1.3579e-33 v ǁVelocityǁ 0.97595 20.021 14.335 17.84 v Pressure 0 0 0 0 v k 0.0014705 2.6401 1.8018 1.6709 v omega 7.3787 28194 1415.8 225.17 v TurbVisc 5.2157e-08 0.13607 0.05243 0.091674 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97621 0.48811 0.48811 INSTANT 0.540000000E+06 TIME STEP NUMBER 540000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99976E+00 0.99976E+00 Friction velocity uk : 0.99976E+00 0.99976E+00 Dimensionless distance yplus : 0.97624E+00 0.97624E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33509E+01 1 0.11336E-08 0.46976E-10 0.42979E-04 c Velocity[X] 0.46976E-10 c Velocity[Y] 0.12972E-31 c Velocity[Z] 0.93341E-65 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20577E+00 1 0.27354E-08 0.18147E-11 0.80317E-04 c omega 0.12990E+03 1 0.16376E-10 0.22184E-09 0.46658E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97601 20.022 14.335 17.841 v Velocity[Y] -8.6647e-17 3.7978e-16 6.3388e-17 1.3251e-16 v Velocity[Z] -9.5119e-33 8.2272e-33 1.7097e-33 6.9504e-34 v ǁVelocityǁ 0.97601 20.022 14.335 17.841 v Pressure 0 0 0 0 v k 0.0014708 2.6403 1.802 1.6711 v omega 7.3791 28194 1415.8 225.17 v TurbVisc 5.2166e-08 0.13608 0.052433 0.091678 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97624 0.48812 0.48812 INSTANT 0.550000000E+06 TIME STEP NUMBER 550000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99979E+00 0.99979E+00 Friction velocity uk : 0.99979E+00 0.99979E+00 Dimensionless distance yplus : 0.97627E+00 0.97627E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33511E+01 1 0.10025E-08 0.36746E-10 0.38011E-04 c Velocity[X] 0.36746E-10 c Velocity[Y] 0.72777E-32 c Velocity[Z] 0.13474E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20580E+00 1 0.24191E-08 0.14196E-11 0.71033E-04 c omega 0.12990E+03 1 0.14484E-10 0.17353E-09 0.41267E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97606 20.022 14.336 17.841 v Velocity[Y] -8.6587e-17 3.2201e-16 5.4478e-17 1.2014e-16 v Velocity[Z] -1.0676e-32 3.638e-33 -3.4233e-34 2.0387e-34 v ǁVelocityǁ 0.97606 20.022 14.336 17.841 v Pressure 0 0 0 0 v k 0.001471 2.6404 1.8021 1.6712 v omega 7.3793 28194 1415.8 225.18 v TurbVisc 5.2174e-08 0.13608 0.052435 0.091682 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97627 0.48814 0.48814 INSTANT 0.560000000E+06 TIME STEP NUMBER 560000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99981E+00 0.99981E+00 Friction velocity uk : 0.99981E+00 0.99981E+00 Dimensionless distance yplus : 0.97630E+00 0.97630E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33513E+01 1 0.88663E-09 0.28744E-10 0.33618E-04 c Velocity[X] 0.28744E-10 c Velocity[Y] 0.12600E-31 c Velocity[Z] 0.27140E-65 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20582E+00 1 0.21395E-08 0.11105E-11 0.62824E-04 c omega 0.12990E+03 1 0.12811E-10 0.13574E-09 0.36499E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97611 20.023 14.336 17.842 v Velocity[Y] -8.7048e-17 3.2804e-16 5.4447e-17 1.196e-16 v Velocity[Z] 2.6052e-56 2.5606e-32 4.8977e-33 1.3674e-33 v ǁVelocityǁ 0.97611 20.023 14.336 17.842 v Pressure 0 0 0 0 v k 0.0014712 2.6406 1.8022 1.6713 v omega 7.3796 28194 1415.8 225.18 v TurbVisc 5.2181e-08 0.13609 0.052437 0.091686 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.9763 0.48815 0.48815 INSTANT 0.570000000E+06 TIME STEP NUMBER 570000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99983E+00 0.99983E+00 Friction velocity uk : 0.99983E+00 0.99983E+00 Dimensionless distance yplus : 0.97632E+00 0.97632E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33515E+01 1 0.78414E-09 0.22484E-10 0.29733E-04 c Velocity[X] 0.22484E-10 c Velocity[Y] 0.40417E-32 c Velocity[Z] 0.22541E-65 c Pressure 0.33410E-51 0 0.10000E+01 -0.33410E-51 0.00000E+00 c k 0.20584E+00 1 0.18921E-08 0.86875E-12 0.55563E-04 c omega 0.12990E+03 1 0.11331E-10 0.10618E-09 0.32282E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97615 20.023 14.337 17.842 v Velocity[Y] -8.6224e-17 3.0497e-16 5.3193e-17 1.1105e-16 v Velocity[Z] 2.6052e-56 2.2994e-32 4.3691e-33 1.2438e-33 v ǁVelocityǁ 0.97615 20.023 14.337 17.842 v Pressure 0 0 0 0 v k 0.0014714 2.6407 1.8023 1.6714 v omega 7.3798 28194 1415.8 225.18 v TurbVisc 5.2188e-08 0.13609 0.052439 0.091689 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97632 0.48816 0.48816 INSTANT 0.580000000E+06 TIME STEP NUMBER 580000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99985E+00 0.99985E+00 Friction velocity uk : 0.99985E+00 0.99985E+00 Dimensionless distance yplus : 0.97634E+00 0.97634E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33517E+01 1 0.69350E-09 0.17588E-10 0.26297E-04 c Velocity[X] 0.17588E-10 c Velocity[Y] 0.10401E-31 c Velocity[Z] 0.12910E-63 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20585E+00 1 0.16734E-08 0.67960E-12 0.49142E-04 c omega 0.12990E+03 1 0.10021E-10 0.83058E-10 0.28552E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97619 20.024 14.337 17.843 v Velocity[Y] -8.6549e-17 2.5635e-16 4.3231e-17 9.7443e-17 v Velocity[Z] 2.6052e-56 1.6727e-32 4.2933e-33 1.2819e-33 v ǁVelocityǁ 0.97619 20.024 14.337 17.843 v Pressure 0 0 0 0 v k 0.0014715 2.6408 1.8024 1.6715 v omega 7.38 28194 1415.8 225.18 v TurbVisc 5.2193e-08 0.1361 0.052441 0.091692 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97634 0.48817 0.48817 INSTANT 0.590000000E+06 TIME STEP NUMBER 590000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99987E+00 0.99987E+00 Friction velocity uk : 0.99987E+00 0.99987E+00 Dimensionless distance yplus : 0.97635E+00 0.97635E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33519E+01 1 0.61334E-09 0.13758E-10 0.23258E-04 c Velocity[X] 0.13758E-10 c Velocity[Y] 0.70026E-32 c Velocity[Z] 0.11122E-63 c Pressure 0.25057E-51 0 0.10000E+01 -0.25057E-51 0.00000E+00 c k 0.20587E+00 1 0.14800E-08 0.53163E-12 0.43463E-04 c omega 0.12990E+03 1 0.88634E-11 0.64972E-10 0.25253E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97623 20.024 14.337 17.843 v Velocity[Y] -8.6777e-17 3.5434e-16 5.8831e-17 1.1895e-16 v Velocity[Z] 2.6052e-56 1.6464e-32 3.762e-33 1.1406e-33 v ǁVelocityǁ 0.97623 20.024 14.337 17.843 v Pressure 0 0 0 0 v k 0.0014717 2.6409 1.8025 1.6716 v omega 7.3802 28194 1415.8 225.18 v TurbVisc 5.2198e-08 0.1361 0.052442 0.091694 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97635 0.48818 0.48818 INSTANT 0.600000000E+06 TIME STEP NUMBER 600000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99988E+00 0.99988E+00 Friction velocity uk : 0.99988E+00 0.99988E+00 Dimensionless distance yplus : 0.97637E+00 0.97637E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33520E+01 1 0.54246E-09 0.10762E-10 0.20571E-04 c Velocity[X] 0.10762E-10 c Velocity[Y] 0.59798E-32 c Velocity[Z] 0.74282E-65 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20588E+00 1 0.13089E-08 0.41588E-12 0.38440E-04 c omega 0.12990E+03 1 0.78393E-11 0.50824E-10 0.22335E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97625 20.025 14.338 17.843 v Velocity[Y] -8.6645e-17 2.9755e-16 4.7985e-17 1.0493e-16 v Velocity[Z] 2.6052e-56 2.9693e-32 4.073e-33 1.1218e-33 v ǁVelocityǁ 0.97625 20.025 14.338 17.843 v Pressure 0 0 0 0 v k 0.0014718 2.641 1.8026 1.6716 v omega 7.3803 28194 1415.8 225.18 v TurbVisc 5.2202e-08 0.13611 0.052444 0.091697 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97637 0.48818 0.48818 INSTANT 0.610000000E+06 TIME STEP NUMBER 610000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99990E+00 0.99990E+00 Friction velocity uk : 0.99990E+00 0.99990E+00 Dimensionless distance yplus : 0.97638E+00 0.97638E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33521E+01 1 0.47976E-09 0.84188E-11 0.18193E-04 c Velocity[X] 0.84188E-11 c Velocity[Y] 0.58118E-32 c Velocity[Z] 0.33983E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20589E+00 1 0.11576E-08 0.32533E-12 0.33998E-04 c omega 0.12990E+03 1 0.69335E-11 0.39757E-10 0.19754E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97628 20.025 14.338 17.843 v Velocity[Y] -8.7044e-17 3.0661e-16 5.0502e-17 1.1007e-16 v Velocity[Z] -1.2346e-32 6.7224e-33 9.1176e-34 5.4838e-34 v ǁVelocityǁ 0.97628 20.025 14.338 17.843 v Pressure 0 0 0 0 v k 0.0014719 2.6411 1.8026 1.6717 v omega 7.3805 28194 1415.8 225.18 v TurbVisc 5.2206e-08 0.13611 0.052445 0.091699 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97638 0.48819 0.48819 INSTANT 0.620000000E+06 TIME STEP NUMBER 620000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99991E+00 0.99991E+00 Friction velocity uk : 0.99991E+00 0.99991E+00 Dimensionless distance yplus : 0.97639E+00 0.97639E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33522E+01 1 0.42432E-09 0.65856E-11 0.16091E-04 c Velocity[X] 0.65856E-11 c Velocity[Y] 0.88101E-32 c Velocity[Z] 0.30366E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20590E+00 1 0.10238E-08 0.25450E-12 0.30069E-04 c omega 0.12990E+03 1 0.61324E-11 0.31100E-10 0.17472E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.9763 20.025 14.338 17.844 v Velocity[Y] -8.8467e-17 2.8185e-16 4.5835e-17 1.0281e-16 v Velocity[Z] -1.1862e-32 8.9336e-33 1.1103e-33 6.0824e-34 v ǁVelocityǁ 0.9763 20.025 14.338 17.844 v Pressure 0 0 0 0 v k 0.001472 2.6412 1.8027 1.6717 v omega 7.3806 28194 1415.8 225.18 v TurbVisc 5.2209e-08 0.13611 0.052446 0.0917 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97639 0.4882 0.4882 INSTANT 0.630000000E+06 TIME STEP NUMBER 630000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99992E+00 0.99992E+00 Friction velocity uk : 0.99992E+00 0.99992E+00 Dimensionless distance yplus : 0.97640E+00 0.97640E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33523E+01 1 0.37528E-09 0.51517E-11 0.14232E-04 c Velocity[X] 0.51517E-11 c Velocity[Y] 0.35111E-32 c Velocity[Z] 0.18484E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20591E+00 1 0.90551E-09 0.19909E-12 0.26594E-04 c omega 0.12990E+03 1 0.54238E-11 0.24328E-10 0.15453E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97632 20.025 14.338 17.844 v Velocity[Y] -9.8017e-17 2.9759e-16 4.9768e-17 1.0626e-16 v Velocity[Z] 2.8879e-55 4.1136e-32 6.991e-33 1.783e-33 v ǁVelocityǁ 0.97632 20.025 14.338 17.844 v Pressure 0 0 0 0 v k 0.0014721 2.6412 1.8027 1.6718 v omega 7.3807 28194 1415.8 225.18 v TurbVisc 5.2212e-08 0.13611 0.052447 0.091702 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.9764 0.4882 0.4882 INSTANT 0.640000000E+06 TIME STEP NUMBER 640000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99993E+00 0.99993E+00 Friction velocity uk : 0.99993E+00 0.99993E+00 Dimensionless distance yplus : 0.97641E+00 0.97641E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33524E+01 1 0.33191E-09 0.40299E-11 0.12587E-04 c Velocity[X] 0.40299E-11 c Velocity[Y] 0.87204E-32 c Velocity[Z] 0.33702E-65 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20592E+00 1 0.80086E-09 0.15574E-12 0.23521E-04 c omega 0.12990E+03 1 0.47971E-11 0.19031E-10 0.13668E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97634 20.026 14.338 17.844 v Velocity[Y] -8.6129e-17 3.1438e-16 5.6314e-17 1.1681e-16 v Velocity[Z] 2.8879e-55 2.987e-32 4.6535e-33 1.252e-33 v ǁVelocityǁ 0.97634 20.026 14.338 17.844 v Pressure 0 0 0 0 v k 0.0014721 2.6413 1.8028 1.6718 v omega 7.3808 28194 1415.8 225.18 v TurbVisc 5.2215e-08 0.13612 0.052447 0.091703 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97641 0.48821 0.48821 INSTANT 0.650000000E+06 TIME STEP NUMBER 650000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99994E+00 0.99994E+00 Friction velocity uk : 0.99994E+00 0.99994E+00 Dimensionless distance yplus : 0.97642E+00 0.97642E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33525E+01 1 0.29356E-09 0.31525E-11 0.11133E-04 c Velocity[X] 0.31525E-11 c Velocity[Y] 0.67086E-32 c Velocity[Z] 0.13492E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20593E+00 1 0.70831E-09 0.12183E-12 0.20803E-04 c omega 0.12990E+03 1 0.42429E-11 0.14887E-10 0.12088E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97636 20.026 14.339 17.844 v Velocity[Y] -8.6183e-17 3.1586e-16 5.8846e-17 1.183e-16 v Velocity[Z] 2.8879e-55 3.5546e-32 5.9776e-33 1.5991e-33 v ǁVelocityǁ 0.97636 20.026 14.339 17.844 v Pressure 0 0 0 0 v k 0.0014722 2.6414 1.8028 1.6719 v omega 7.3809 28194 1415.8 225.18 v TurbVisc 5.2217e-08 0.13612 0.052448 0.091704 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97642 0.48821 0.48821 INSTANT 0.660000000E+06 TIME STEP NUMBER 660000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99994E+00 0.99994E+00 Friction velocity uk : 0.99994E+00 0.99994E+00 Dimensionless distance yplus : 0.97643E+00 0.97643E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33525E+01 1 0.25964E-09 0.24660E-11 0.98465E-05 c Velocity[X] 0.24660E-11 c Velocity[Y] 0.97437E-32 c Velocity[Z] 0.20272E-65 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20593E+00 1 0.62646E-09 0.95305E-13 0.18400E-04 c omega 0.12990E+03 1 0.37526E-11 0.11646E-10 0.10692E-06 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97637 20.026 14.339 17.844 v Velocity[Y] -8.6954e-17 3.7767e-16 6.7514e-17 1.3098e-16 v Velocity[Z] -1.5309e-33 7.603e-33 1.5331e-33 5.9265e-34 v ǁVelocityǁ 0.97637 20.026 14.339 17.844 v Pressure 0 0 0 0 v k 0.0014723 2.6414 1.8029 1.6719 v omega 7.3809 28194 1415.8 225.18 v TurbVisc 5.222e-08 0.13612 0.052449 0.091705 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97643 0.48821 0.48821 INSTANT 0.670000000E+06 TIME STEP NUMBER 670000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99995E+00 0.99995E+00 Friction velocity uk : 0.99995E+00 0.99995E+00 Dimensionless distance yplus : 0.97643E+00 0.97643E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33526E+01 1 0.22963E-09 0.19291E-11 0.87088E-05 c Velocity[X] 0.19291E-11 c Velocity[Y] 0.76190E-32 c Velocity[Z] 0.12731E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20594E+00 1 0.55407E-09 0.74554E-13 0.16274E-04 c omega 0.12990E+03 1 0.33191E-11 0.91101E-11 0.94564E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97638 20.026 14.339 17.845 v Velocity[Y] -9.3647e-17 3.2886e-16 5.346e-17 1.2052e-16 v Velocity[Z] 2.8879e-55 1.2585e-32 3.1568e-33 9.6347e-34 v ǁVelocityǁ 0.97638 20.026 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014723 2.6414 1.8029 1.6719 v omega 7.381 28194 1415.8 225.18 v TurbVisc 5.2221e-08 0.13612 0.052449 0.091706 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97643 0.48822 0.48822 INSTANT 0.680000000E+06 TIME STEP NUMBER 680000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99996E+00 0.99996E+00 Friction velocity uk : 0.99996E+00 0.99996E+00 Dimensionless distance yplus : 0.97644E+00 0.97644E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33526E+01 1 0.20310E-09 0.15091E-11 0.77025E-05 c Velocity[X] 0.15091E-11 c Velocity[Y] 0.76873E-32 c Velocity[Z] 0.13480E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20594E+00 1 0.49004E-09 0.58322E-13 0.14393E-04 c omega 0.12990E+03 1 0.29356E-11 0.71265E-11 0.83638E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.9764 20.026 14.339 17.845 v Velocity[Y] -8.6914e-17 4.2018e-16 6.2348e-17 1.3172e-16 v Velocity[Z] 2.8879e-55 1.9868e-32 2.6263e-33 8.0952e-34 v ǁVelocityǁ 0.9764 20.026 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014724 2.6415 1.8029 1.6719 v omega 7.3811 28194 1415.8 225.18 v TurbVisc 5.2223e-08 0.13612 0.05245 0.091707 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97644 0.48822 0.48822 INSTANT 0.690000000E+06 TIME STEP NUMBER 690000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99996E+00 0.99996E+00 Friction velocity uk : 0.99996E+00 0.99996E+00 Dimensionless distance yplus : 0.97644E+00 0.97644E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33527E+01 1 0.17963E-09 0.11805E-11 0.68126E-05 c Velocity[X] 0.11805E-11 c Velocity[Y] 0.61957E-32 c Velocity[Z] 0.16205E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20595E+00 1 0.43342E-09 0.45624E-13 0.12730E-04 c omega 0.12990E+03 1 0.25964E-11 0.55748E-11 0.73975E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97641 20.026 14.339 17.845 v Velocity[Y] -8.6638e-17 3.5632e-16 5.5038e-17 1.1934e-16 v Velocity[Z] 2.8879e-55 1.748e-32 4.1352e-33 1.1738e-33 v ǁVelocityǁ 0.97641 20.026 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014724 2.6415 1.8029 1.672 v omega 7.3811 28194 1415.8 225.18 v TurbVisc 5.2224e-08 0.13612 0.05245 0.091708 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97644 0.48822 0.48822 INSTANT 0.700000000E+06 TIME STEP NUMBER 700000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99997E+00 0.99997E+00 Friction velocity uk : 0.99997E+00 0.99997E+00 Dimensionless distance yplus : 0.97645E+00 0.97645E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33527E+01 1 0.15887E-09 0.92346E-12 0.60254E-05 c Velocity[X] 0.92346E-12 c Velocity[Y] 0.61757E-32 c Velocity[Z] 0.12470E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20595E+00 1 0.38333E-09 0.35690E-13 0.11259E-04 c omega 0.12990E+03 1 0.22964E-11 0.43610E-11 0.65428E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97641 20.027 14.339 17.845 v Velocity[Y] -9.3647e-17 4.3029e-16 6.7674e-17 1.3608e-16 v Velocity[Z] 5.7547e-55 1.2568e-32 3.0614e-33 9.5569e-34 v ǁVelocityǁ 0.97641 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014724 2.6415 1.803 1.672 v omega 7.3811 28194 1415.8 225.18 v TurbVisc 5.2226e-08 0.13612 0.05245 0.091709 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97645 0.48822 0.48822 INSTANT 0.710000000E+06 TIME STEP NUMBER 710000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99997E+00 0.99997E+00 Friction velocity uk : 0.99997E+00 0.99997E+00 Dimensionless distance yplus : 0.97645E+00 0.97645E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33527E+01 1 0.14052E-09 0.72240E-12 0.53292E-05 c Velocity[X] 0.72240E-12 c Velocity[Y] 0.10486E-31 c Velocity[Z] 0.98299E-66 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20595E+00 1 0.33904E-09 0.27920E-13 0.99583E-05 c omega 0.12990E+03 1 0.20311E-11 0.34115E-11 0.57868E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97642 20.027 14.339 17.845 v Velocity[Y] -8.6222e-17 4.1924e-16 7.0584e-17 1.3916e-16 v Velocity[Z] 5.7547e-55 1.9858e-32 3.5575e-33 1.0034e-33 v ǁVelocityǁ 0.97642 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014725 2.6416 1.803 1.672 v omega 7.3812 28194 1415.8 225.18 v TurbVisc 5.2227e-08 0.13613 0.052451 0.091709 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97645 0.48823 0.48823 INSTANT 0.720000000E+06 TIME STEP NUMBER 720000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99997E+00 0.99997E+00 Friction velocity uk : 0.99997E+00 0.99997E+00 Dimensionless distance yplus : 0.97645E+00 0.97645E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33528E+01 1 0.12428E-09 0.56511E-12 0.47135E-05 c Velocity[X] 0.56511E-12 c Velocity[Y] 0.67466E-32 c Velocity[Z] 0.12756E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20596E+00 1 0.29986E-09 0.21841E-13 0.88077E-05 c omega 0.12990E+03 1 0.17964E-11 0.26687E-11 0.51182E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97643 20.027 14.339 17.845 v Velocity[Y] -8.6861e-17 3.9986e-16 6.5027e-17 1.269e-16 v Velocity[Z] 5.7547e-55 3.6691e-32 6.0988e-33 1.5789e-33 v ǁVelocityǁ 0.97643 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014725 2.6416 1.803 1.672 v omega 7.3812 28194 1415.8 225.18 v TurbVisc 5.2228e-08 0.13613 0.052451 0.09171 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97645 0.48823 0.48823 INSTANT 0.730000000E+06 TIME STEP NUMBER 730000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99998E+00 0.99998E+00 Friction velocity uk : 0.99998E+00 0.99998E+00 Dimensionless distance yplus : 0.97646E+00 0.97646E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33528E+01 1 0.10992E-09 0.44207E-12 0.41689E-05 c Velocity[X] 0.44207E-12 c Velocity[Y] 0.48981E-32 c Velocity[Z] 0.12458E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20596E+00 1 0.26522E-09 0.17086E-13 0.77900E-05 c omega 0.12990E+03 1 0.15889E-11 0.20876E-11 0.45269E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97643 20.027 14.339 17.845 v Velocity[Y] -8.7046e-17 3.7764e-16 6.0225e-17 1.2886e-16 v Velocity[Z] 5.7547e-55 2.5145e-32 4.6308e-33 1.2007e-33 v ǁVelocityǁ 0.97643 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014725 2.6416 1.803 1.672 v omega 7.3813 28194 1415.8 225.18 v TurbVisc 5.2229e-08 0.13613 0.052451 0.09171 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97646 0.48823 0.48823 INSTANT 0.740000000E+06 TIME STEP NUMBER 740000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99998E+00 0.99998E+00 Friction velocity uk : 0.99998E+00 0.99998E+00 Dimensionless distance yplus : 0.97646E+00 0.97646E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33528E+01 1 0.97221E-10 0.34582E-12 0.36872E-05 c Velocity[X] 0.34582E-12 c Velocity[Y] 0.30735E-32 c Velocity[Z] 0.13488E-63 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20596E+00 1 0.23457E-09 0.13366E-13 0.68900E-05 c omega 0.12990E+03 1 0.14053E-11 0.16331E-11 0.40039E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97644 20.027 14.339 17.845 v Velocity[Y] -8.6405e-17 3.8418e-16 6.4634e-17 1.3595e-16 v Velocity[Z] 5.7547e-55 1.9175e-32 4.3521e-33 1.2541e-33 v ǁVelocityǁ 0.97644 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014725 2.6416 1.803 1.672 v omega 7.3813 28194 1415.8 225.18 v TurbVisc 5.2229e-08 0.13613 0.052451 0.091711 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97646 0.48823 0.48823 INSTANT 0.750000000E+06 TIME STEP NUMBER 750000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99998E+00 0.99998E+00 Friction velocity uk : 0.99998E+00 0.99998E+00 Dimensionless distance yplus : 0.97646E+00 0.97646E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 750000, Physical time 0.75000E+06 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 750000: 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 0.33528E+01 1 0.85987E-10 0.27052E-12 0.32612E-05 c Velocity[X] 0.27052E-12 c Velocity[Y] 0.50411E-32 c Velocity[Z] 0.13489E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20596E+00 1 0.20747E-09 0.10456E-13 0.60939E-05 c omega 0.12990E+03 1 0.12429E-11 0.12775E-11 0.35413E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97644 20.027 14.339 17.845 v Velocity[Y] -8.9278e-17 3.9694e-16 6.3168e-17 1.3271e-16 v Velocity[Z] 5.7547e-55 1.8633e-32 4.2895e-33 1.2595e-33 v ǁVelocityǁ 0.97644 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014726 2.6416 1.803 1.672 v omega 7.3813 28194 1415.8 225.18 v TurbVisc 5.223e-08 0.13613 0.052452 0.091711 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97646 0.48823 0.48823 INSTANT 0.760000000E+06 TIME STEP NUMBER 760000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99998E+00 0.99998E+00 Friction velocity uk : 0.99998E+00 0.99998E+00 Dimensionless distance yplus : 0.97646E+00 0.97646E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.76052E-10 0.21162E-12 0.28844E-05 c Velocity[X] 0.21162E-12 c Velocity[Y] 0.62569E-32 c Velocity[Z] 0.12518E-63 c Pressure 0.50114E-51 0 0.10000E+01 -0.50114E-51 0.00000E+00 c k 0.20597E+00 1 0.18350E-09 0.81791E-14 0.53898E-05 c omega 0.12990E+03 1 0.10993E-11 0.99937E-12 0.31321E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97645 20.027 14.339 17.845 v Velocity[Y] -8.6222e-17 3.6033e-16 6.3563e-17 1.3012e-16 v Velocity[Z] -1.9356e-32 3.1706e-33 -1.1636e-33 4.4319e-35 v ǁVelocityǁ 0.97645 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014726 2.6416 1.803 1.6721 v omega 7.3813 28194 1415.8 225.18 v TurbVisc 5.2231e-08 0.13613 0.052452 0.091711 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97646 0.48823 0.48823 INSTANT 0.770000000E+06 TIME STEP NUMBER 770000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97647E+00 0.97647E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.67265E-10 0.16555E-12 0.25511E-05 c Velocity[X] 0.16555E-12 c Velocity[Y] 0.10527E-31 c Velocity[Z] 0.12570E-63 c Pressure 0.20881E-52 0 0.10000E+01 -0.20881E-52 0.00000E+00 c k 0.20597E+00 1 0.16230E-09 0.63983E-14 0.47671E-05 c omega 0.12990E+03 1 0.97231E-12 0.78178E-12 0.27702E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97645 20.027 14.339 17.845 v Velocity[Y] -8.6645e-17 3.4751e-16 5.5058e-17 1.2372e-16 v Velocity[Z] 1.1488e-54 5.9539e-33 1.7957e-33 6.9503e-34 v ǁVelocityǁ 0.97645 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014726 2.6417 1.803 1.6721 v omega 7.3813 28194 1415.8 225.18 v TurbVisc 5.2231e-08 0.13613 0.052452 0.091711 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97647 0.48823 0.48823 INSTANT 0.780000000E+06 TIME STEP NUMBER 780000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97647E+00 0.97647E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.59493E-10 0.12950E-12 0.22564E-05 c Velocity[X] 0.12950E-12 c Velocity[Y] 0.41489E-32 c Velocity[Z] 0.12610E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20597E+00 1 0.14354E-09 0.50053E-14 0.42163E-05 c omega 0.12990E+03 1 0.85997E-12 0.61157E-12 0.24502E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97646 20.027 14.339 17.845 v Velocity[Y] -8.677e-17 3.8579e-16 6.2421e-17 1.2825e-16 v Velocity[Z] 1.1488e-54 8.8383e-33 2.1651e-33 6.8256e-34 v ǁVelocityǁ 0.97646 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014726 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2232e-08 0.13613 0.052452 0.091712 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97647 0.48823 0.48823 INSTANT 0.790000000E+06 TIME STEP NUMBER 790000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97647E+00 0.97647E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.52619E-10 0.10131E-12 0.19957E-05 c Velocity[X] 0.10131E-12 c Velocity[Y] 0.37174E-32 c Velocity[Z] 0.50471E-66 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20597E+00 1 0.12696E-09 0.39155E-14 0.37291E-05 c omega 0.12990E+03 1 0.76061E-12 0.47841E-12 0.21671E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97646 20.027 14.339 17.845 v Velocity[Y] -8.6549e-17 4.7193e-16 7.7632e-17 1.483e-16 v Velocity[Z] 1.4355e-54 1.7396e-32 3.7549e-33 1.0853e-33 v ǁVelocityǁ 0.97646 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014726 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2232e-08 0.13613 0.052452 0.091712 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97647 0.48823 0.48823 INSTANT 0.800000000E+06 TIME STEP NUMBER 800000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97647E+00 0.97647E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.46540E-10 0.79249E-13 0.17651E-05 c Velocity[X] 0.79249E-13 c Velocity[Y] 0.29413E-32 c Velocity[Z] 0.65967E-66 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20597E+00 1 0.11229E-09 0.30630E-14 0.32983E-05 c omega 0.12990E+03 1 0.67273E-12 0.37425E-12 0.19167E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97646 20.027 14.339 17.845 v Velocity[Y] -8.6774e-17 3.7568e-16 6.5862e-17 1.3134e-16 v Velocity[Z] 1.4355e-54 3.9261e-32 7.4634e-33 1.9172e-33 v ǁVelocityǁ 0.97646 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014726 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2232e-08 0.13613 0.052452 0.091712 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97647 0.48824 0.48824 INSTANT 0.810000000E+06 TIME STEP NUMBER 810000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97647E+00 0.97647E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.41163E-10 0.61994E-13 0.15612E-05 c Velocity[X] 0.61994E-13 c Velocity[Y] 0.50397E-32 c Velocity[Z] 0.50113E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20597E+00 1 0.99316E-10 0.23961E-14 0.29172E-05 c omega 0.12990E+03 1 0.59501E-12 0.29277E-12 0.16953E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97646 20.027 14.339 17.845 v Velocity[Y] -1.0232e-16 3.6693e-16 6.3395e-17 1.2536e-16 v Velocity[Z] -6.0907e-33 9.8687e-33 1.9764e-33 7.5895e-34 v ǁVelocityǁ 0.97646 20.027 14.339 17.845 v Pressure 0 0 0 0 v k 0.0014726 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2233e-08 0.13613 0.052452 0.091712 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97647 0.48824 0.48824 INSTANT 0.820000000E+06 TIME STEP NUMBER 820000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97647E+00 0.97647E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.36407E-10 0.48497E-13 0.13808E-05 c Velocity[X] 0.48497E-13 c Velocity[Y] 0.18872E-31 c Velocity[Z] 0.20957E-65 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20597E+00 1 0.87841E-10 0.18744E-14 0.25801E-05 c omega 0.12990E+03 1 0.52626E-12 0.22902E-12 0.14994E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.845 v Velocity[Y] -8.6872e-17 3.5435e-16 6.0253e-17 1.227e-16 v Velocity[Z] 1.4355e-54 1.2897e-32 3.2787e-33 1.0303e-33 v ǁVelocityǁ 0.97647 20.027 14.34 17.845 v Pressure 0 0 0 0 v k 0.0014726 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2233e-08 0.13613 0.052453 0.091712 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97647 0.48824 0.48824 INSTANT 0.830000000E+06 TIME STEP NUMBER 830000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97647E+00 0.97647E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.32200E-10 0.37938E-13 0.12213E-05 c Velocity[X] 0.37938E-13 c Velocity[Y] 0.70553E-32 c Velocity[Z] 0.57363E-65 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20597E+00 1 0.77692E-10 0.14663E-14 0.22820E-05 c omega 0.12990E+03 1 0.46546E-12 0.17916E-12 0.13262E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.845 v Velocity[Y] -8.6405e-17 3.4382e-16 6.5902e-17 1.2318e-16 v Velocity[Z] 1.4355e-54 2.2174e-32 4.2318e-33 1.1605e-33 v ǁVelocityǁ 0.97647 20.027 14.34 17.845 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2233e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97647 0.48824 0.48824 INSTANT 0.840000000E+06 TIME STEP NUMBER 840000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97647E+00 0.97647E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33529E+01 1 0.28480E-10 0.29678E-13 0.10802E-05 c Velocity[X] 0.29678E-13 c Velocity[Y] 0.60457E-32 c Velocity[Z] 0.16859E-66 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20598E+00 1 0.68715E-10 0.11471E-14 0.20184E-05 c omega 0.12990E+03 1 0.41168E-12 0.14015E-12 0.11729E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.845 v Velocity[Y] -8.6403e-17 3.6751e-16 6.3089e-17 1.2542e-16 v Velocity[Z] -1.3225e-32 7.1158e-33 3.9793e-34 4.7365e-34 v ǁVelocityǁ 0.97647 20.027 14.34 17.845 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2234e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97647 0.48824 0.48824 INSTANT 0.850000000E+06 TIME STEP NUMBER 850000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99999E+00 0.99999E+00 Friction velocity uk : 0.99999E+00 0.99999E+00 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.25189E-10 0.23216E-13 0.95536E-06 c Velocity[X] 0.23216E-13 c Velocity[Y] 0.56333E-32 c Velocity[Z] 0.12693E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20598E+00 1 0.60776E-10 0.89732E-15 0.17852E-05 c omega 0.12990E+03 1 0.36412E-12 0.10964E-12 0.10374E-07 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.846 v Velocity[Y] -9.7949e-17 3.7482e-16 7.2611e-17 1.41e-16 v Velocity[Z] -2.7097e-33 1.6498e-32 3.3212e-33 1.0684e-33 v ǁVelocityǁ 0.97647 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2234e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.860000000E+06 TIME STEP NUMBER 860000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.22279E-10 0.18161E-13 0.84498E-06 c Velocity[X] 0.18161E-13 c Velocity[Y] 0.80324E-32 c Velocity[Z] 0.13391E-65 c Pressure 0.83524E-52 0 0.10000E+01 -0.83524E-52 0.00000E+00 c k 0.20598E+00 1 0.53754E-10 0.70195E-15 0.15789E-05 c omega 0.12990E+03 1 0.32205E-12 0.85766E-13 0.91756E-08 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.846 v Velocity[Y] -8.618e-17 3.858e-16 6.7711e-17 1.409e-16 v Velocity[Z] -1.5419e-33 7.3868e-33 1.7103e-33 6.9696e-34 v ǁVelocityǁ 0.97647 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2234e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.870000000E+06 TIME STEP NUMBER 870000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.19705E-10 0.14207E-13 0.74735E-06 c Velocity[X] 0.14207E-13 c Velocity[Y] 0.94145E-32 c Velocity[Z] 0.12994E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20598E+00 1 0.47543E-10 0.54912E-15 0.13965E-05 c omega 0.12990E+03 1 0.28484E-12 0.67093E-13 0.81155E-08 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.846 v Velocity[Y] -8.6312e-17 3.8682e-16 6.5641e-17 1.3797e-16 v Velocity[Z] 2.0089e-54 2.3809e-32 4.4569e-33 1.2625e-33 v ǁVelocityǁ 0.97647 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2234e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.880000000E+06 TIME STEP NUMBER 880000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.17426E-10 0.11113E-13 0.66096E-06 c Velocity[X] 0.11113E-13 c Velocity[Y] 0.74749E-32 c Velocity[Z] 0.10207E-65 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20598E+00 1 0.42194E-10 0.43274E-15 0.12396E-05 c omega 0.12990E+03 1 0.25743E-12 0.55793E-13 0.73858E-08 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.846 v Velocity[Y] -8.8464e-17 4.1815e-16 7.3141e-17 1.3672e-16 v Velocity[Z] 2.0089e-54 1.8488e-32 3.7809e-33 1.0957e-33 v ǁVelocityǁ 0.97647 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3814 28194 1415.8 225.18 v TurbVisc 5.2234e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.890000000E+06 TIME STEP NUMBER 890000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.15388E-10 0.86826E-14 0.58399E-06 c Velocity[X] 0.86826E-14 c Velocity[Y] 0.99796E-32 c Velocity[Z] 0.14139E-63 c Pressure 0.43373E-18 0 0.10000E+01 -0.43373E-18 0.00000E+00 c k 0.20598E+00 1 0.37890E-10 0.34535E-15 0.11095E-05 c omega 0.12990E+03 1 0.25963E-12 0.58339E-13 0.74871E-08 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.846 v Velocity[Y] -8.618e-17 4.405e-16 7.7522e-17 1.4482e-16 v Velocity[Z] 2.0089e-54 1.5537e-32 3.5154e-33 1.0622e-33 v ǁVelocityǁ 0.97647 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.18 v TurbVisc 5.2234e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.900000000E+06 TIME STEP NUMBER 900000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.13594E-10 0.67808E-14 0.51602E-06 c Velocity[X] 0.67808E-14 c Velocity[Y] 0.24587E-32 c Velocity[Z] 0.12678E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20598E+00 1 0.33482E-10 0.26919E-15 0.97966E-06 c omega 0.12990E+03 1 0.26264E-12 0.60769E-13 0.75493E-08 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97647 20.027 14.34 17.846 v Velocity[Y] -8.6729e-17 3.8033e-16 6.2421e-17 1.3134e-16 v Velocity[Z] 2.0089e-54 3.6237e-32 6.5324e-33 1.7036e-33 v ǁVelocityǁ 0.97647 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.18 v TurbVisc 5.2234e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.910000000E+06 TIME STEP NUMBER 910000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.12013E-10 0.52958E-14 0.45603E-06 c Velocity[X] 0.52958E-14 c Velocity[Y] 0.97632E-32 c Velocity[Z] 0.13305E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20598E+00 1 0.29528E-10 0.20950E-15 0.86411E-06 c omega 0.12990E+03 1 0.25746E-12 0.57306E-13 0.74459E-08 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.8464e-17 3.3893e-16 6.1309e-17 1.2404e-16 v Velocity[Z] -9.4034e-33 1.2204e-32 2.2937e-33 8.7026e-34 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.18 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.920000000E+06 TIME STEP NUMBER 920000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.10617E-10 0.41363E-14 0.40303E-06 c Velocity[X] 0.41363E-14 c Velocity[Y] 0.92282E-32 c Velocity[Z] 0.13124E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20598E+00 1 0.26092E-10 0.16372E-15 0.76378E-06 c omega 0.12990E+03 1 0.26086E-12 0.59625E-13 0.75160E-08 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.6274e-17 3.0487e-16 5.9626e-17 1.1217e-16 v Velocity[Z] 2.0089e-54 1.5925e-32 4.0109e-33 1.1703e-33 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.18 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.930000000E+06 TIME STEP NUMBER 930000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.93828E-11 0.32306E-14 0.35618E-06 c Velocity[X] 0.32306E-14 c Velocity[Y] 0.73751E-32 c Velocity[Z] 0.13441E-63 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20598E+00 1 0.23074E-10 0.12800E-15 0.67542E-06 c omega 0.12990E+03 0 0.99942E-12 0.00000E+00 0.00000E+00 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.8464e-17 3.4138e-16 5.8039e-17 1.1916e-16 v Velocity[Z] -2.717e-33 4.8439e-33 1.1656e-33 5.5256e-34 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.18 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.940000000E+06 TIME STEP NUMBER 940000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.82932E-11 0.25235E-14 0.31480E-06 c Velocity[X] 0.25235E-14 c Velocity[Y] 0.59508E-32 c Velocity[Z] 0.87168E-66 c Pressure 0.10440E-51 0 0.10000E+01 -0.10440E-51 0.00000E+00 c k 0.20598E+00 1 0.20363E-10 0.99733E-16 0.59617E-06 c omega 0.12990E+03 0 0.98552E-12 0.00000E+00 0.00000E+00 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.6592e-17 3.098e-16 5.3289e-17 1.0866e-16 v Velocity[Z] -1.7611e-33 6.2292e-33 1.5994e-33 6.607e-34 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.18 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.950000000E+06 TIME STEP NUMBER 950000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.73290E-11 0.19709E-14 0.27820E-06 c Velocity[X] 0.19709E-14 c Velocity[Y] 0.40000E-32 c Velocity[Z] 0.13111E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20598E+00 1 0.18018E-10 0.78020E-16 0.52737E-06 c omega 0.12990E+03 0 0.98669E-12 0.00000E+00 0.00000E+00 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.6276e-17 4.0506e-16 7.1299e-17 1.4054e-16 v Velocity[Z] 2.1459e-54 3.0252e-32 5.0701e-33 1.3649e-33 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.18 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.960000000E+06 TIME STEP NUMBER 960000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.64772E-11 0.15394E-14 0.24587E-06 c Velocity[X] 0.15394E-14 c Velocity[Y] 0.75954E-32 c Velocity[Z] 0.17929E-65 c Pressure 0.27145E-51 0 0.10000E+01 -0.27145E-51 0.00000E+00 c k 0.20598E+00 1 0.15917E-10 0.60894E-16 0.46589E-06 c omega 0.12990E+03 0 0.98527E-12 0.00000E+00 0.00000E+00 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.659e-17 4.4557e-16 7.3456e-17 1.4162e-16 v Velocity[Z] -5.7653e-33 1.3108e-32 2.3873e-33 9.1626e-34 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.19 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.970000000E+06 TIME STEP NUMBER 970000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.57246E-11 0.12024E-14 0.21730E-06 c Velocity[X] 0.12024E-14 c Velocity[Y] 0.76032E-32 c Velocity[Z] 0.53000E-65 c Pressure 0.16705E-51 0 0.10000E+01 -0.16705E-51 0.00000E+00 c k 0.20598E+00 1 0.14058E-10 0.47568E-16 0.41161E-06 c omega 0.12990E+03 1 0.25794E-12 0.57899E-13 0.74474E-08 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.6221e-17 3.725e-16 6.5164e-17 1.321e-16 v Velocity[Z] 2.1459e-54 2.1613e-32 4.771e-33 1.3539e-33 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.19 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.980000000E+06 TIME STEP NUMBER 980000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.50592E-11 0.93914E-15 0.19204E-06 c Velocity[X] 0.93914E-15 c Velocity[Y] 0.15184E-32 c Velocity[Z] 0.12755E-63 c Pressure 0.00000E+00 0 0.00000E+00 -0.00000E+00 0.00000E+00 c k 0.20598E+00 1 0.12431E-10 0.37151E-16 0.36386E-06 c omega 0.12990E+03 0 0.99099E-12 0.00000E+00 0.00000E+00 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.6456e-17 3.6552e-16 6.2566e-17 1.3252e-16 v Velocity[Z] 2.1459e-54 2.2717e-32 4.4787e-33 1.2602e-33 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.19 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 INSTANT 0.990000000E+06 TIME STEP NUMBER 990000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33530E+01 1 0.44711E-11 0.73352E-15 0.16972E-06 c Velocity[X] 0.73352E-15 c Velocity[Y] 0.58492E-32 c Velocity[Z] 0.37258E-66 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20598E+00 1 0.10982E-10 0.28987E-16 0.32140E-06 c omega 0.12990E+03 0 0.99523E-12 0.00000E+00 0.00000E+00 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -1.1092e-16 4.1711e-16 7.0806e-17 1.3801e-16 v Velocity[Z] 2.1459e-54 1.9182e-32 4.2163e-33 1.1997e-33 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.19 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- INSTANT 0.100000000E+07 TIME STEP NUMBER 1000000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 1 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10000E+01 0.10000E+01 Friction velocity uk : 0.10000E+01 0.10000E+01 Dimensionless distance yplus : 0.97648E+00 0.97648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 1 ------------------------------------------------------------ Write final restart files checkpoint at iteration 1000000, Physical time 0.10000E+07 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 1000000: 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 0.33530E+01 1 0.39515E-11 0.57294E-15 0.15000E-06 c Velocity[X] 0.57294E-15 c Velocity[Y] 0.23720E-32 c Velocity[Z] 0.81681E-65 c Pressure 0.43368E-18 0 0.10000E+01 -0.43368E-18 0.00000E+00 c k 0.20598E+00 1 0.97076E-11 0.22650E-16 0.28414E-06 c omega 0.12990E+03 0 0.98298E-12 0.00000E+00 0.00000E+00 c Wall distance 0.25634E-04 16 0.98844E-08 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** "Clippings" des champs calculés ------------------------------- champ min. init. max. init. lim. à min. lim. à max. - ----- -------------- -------------- ------------ ------------ a k a omega ** Champs calculés sur cellules ---------------------------- champ minimum maximum moy. ensemble moy. spatiale - -------------- -------------- -------------- -------------- -------------- v Velocity[X] 0.97648 20.027 14.34 17.846 v Velocity[Y] -8.6271e-17 3.4138e-16 7.038e-17 1.349e-16 v Velocity[Z] -5.1693e-33 5.751e-33 7.8391e-34 4.5837e-34 v ǁVelocityǁ 0.97648 20.027 14.34 17.846 v Pressure 0 0 0 0 v k 0.0014727 2.6417 1.8031 1.6721 v omega 7.3815 28194 1415.8 225.19 v TurbVisc 5.2235e-08 0.13613 0.052453 0.091713 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Wall distance 0.0024926 0.94206 0.26542 0.50069 ** Champs calculés sur faces de bord --------------------------------- champ minimum maximum moy. ensemble moy. spatiale - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.97648 0.48824 0.48824 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destruction des structures et clôture du calcul