command: ./cs_solver --mpi *************************************************************** (R) Code_Saturne Version 6.0.5 Copyright (C) 1998-2019 EDF S.A., France revision 6.0.5-3e9e9e94c build sam. 21 nov. 2020 14:36:04 CET MPI version 3.1 (Open MPI 2.1.1) The Code_Saturne CFD tool is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 2 of the License, or (at your option) any later version. The Code_Saturne CFD tool is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. *************************************************************** Local case configuration: Date: mer. 01 sept. 2021 12:35:02 CEST System: Linux 5.4.0-81-generic (Ubuntu 18.04.5 LTS) Machine: tsubasa-VirtualBox Processor: model name : Intel(R) Core(TM) i7-10610U CPU @ 1.80GHz Memory: 7962 MB User: tsubasa (tsubasa) Directory: /home/tsubasa/Desktop/mesh_convergence/test_masflx/RESU/20210901-1235 MPI ranks: 4 (appnum attribute: 0) OpenMP threads: 1 Processors/node: 1 I/O read method: collective MPI-IO (explicit offsets) I/O write method: collective MPI-IO (explicit offsets) I/O rank step: 1 External libraries for partitioning: ParMETIS 4.0.3 PT-SCOTCH 6.0.9 Reading metadata from file: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: IN THE DATA SPECIFICATION @ ======== @ @ The k-omega turbulence model has been chosen. In order to @ have a correct calculation restart, the ICDPAR indicator @ has been set to 1 (read the wall distance in the restart @ file). @ If this initialization raises any issue (modification of, @ the number and position of the wall faces since the @ previous calcuation), force ICDPAR=1 (there might be, @ a small shift in the turbulent viscosity at the, @ first time-step)., @ @ The calculation will be run. @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 9 (Nb variables ) NSCAL = 2 (Nb scalars ) NSCAUS = 2 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) ----------------------------------------------------------- ** HOMOGENEOUS MIXTURE MODEL VoF ---------------------------------------- IVOFMT = 0 ( 0 : disabled ) ( > 0: enabled ) ----------------------------------------------------------- ** TIME STEPPING ------------- --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Velocity 1 0.1000E+01 Pressure 0 0.1000E+01 k 1 0.1000E+01 omega 1 0.1000E+01 scalar1 1 0.1000E+01 variance1 1 0.1000E+01 Wall distance 0 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** STOKES ------ -- 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 ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) ------------------------------------------------------------- Variable Number ISCACP ITURT VISLS0 SIGMAS ------------------------------------------------------------- scalar1 1 0 0 0.2157E-04 0.1000E+01 variance1 2 0 0 0.2157E-04 0.1000E+01 ------------------------------------------------------------- ------------------------------------ Variable Number RVARFL ------------------------------------ scalar1 1 0.8000E+00 variance1 2 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- scalar1 1 -1 -0.1000E+13 0.1000E+13 variance1 2 0 -0.1000E+13 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. ISCACP = 0 or 1 2 (use Cp or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 or 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS THETVS ------------------------------------------------------ 1 0.0000E+00 0.0000E+00 2 0.0000E+00 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 1 (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 = 500 (Initial time step) NTMABS = 520 (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 = 1 (Output frequency ) -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted by the fluid on the boundary) ipstyp = 0 (y+ at boundary) ipsttp = 0 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 0 (Dimensionless thermal flux at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated,2: CDO ) NALINF = 0 (Fluid initialization iterations) IFLXMW = 0 (ALE mass flux computation 0: thanks to vertices 1: thanks to mesh velocity) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: time dependency: fixed mesh output: every 1 time steps and at calculation end -5: name: directory: monitoring format: time_plot options: time dependency: fixed mesh output: every 1 time steps -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at calculation end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at calculation end Reading file: mesh_input Finished reading: mesh_input No "partition_input/domain_number_4" file available; ---------------------------------------------------------- Partitioning 75699 cells to 4 domains on 4 ranks (SCOTCH_dgraphPart). wall-clock time: 0.601133 s Number of cells per domain (histogramm): [ 18478 ; 18578 [ = 1 [ 18578 ; 18679 [ = 0 [ 18679 ; 18779 [ = 1 [ 18779 ; 18880 [ = 0 [ 18880 ; 18981 [ = 0 [ 18981 ; 19081 [ = 1 [ 19081 ; 19182 [ = 0 [ 19182 ; 19282 [ = 0 [ 19282 ; 19383 [ = 0 [ 19383 ; 19484 ] = 1 Writing file: partition_output/domain_number_4 Finished writing: partition_output/domain_number_4 Partitioning finished (0.77 s) ---------------------------------------------------------- Halo construction with standard neighborhood ============================================ Face interfaces creation Vertex interfaces creation Halo creation Halo definition Local halo definition Distant halo creation Updating the faces -> cells connectivity Histogram of the number of cells per rank: minimum value = 18478 maximum value = 19484 1 : [ 18478 ; 18679 [ = 1 2 : [ 18679 ; 18880 [ = 1 3 : [ 18880 ; 19081 [ = 1 4 : [ 19081 ; 19282 [ = 0 5 : [ 19282 ; 19484 ] = 1 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 19452 maximum value = 20202 1 : [ 19452 ; 19602 [ = 2 2 : [ 19602 ; 19752 [ = 0 3 : [ 19752 ; 19902 [ = 1 4 : [ 19902 ; 20052 [ = 0 5 : [ 20052 ; 20202 ] = 1 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 718 maximum value = 989 1 : [ 718 ; 772 [ = 3 2 : [ 772 ; 826 [ = 0 3 : [ 826 ; 880 [ = 0 4 : [ 880 ; 934 [ = 0 5 : [ 934 ; 989 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 36536 maximum value = 39938 1 : [ 36536 ; 37216 [ = 2 2 : [ 37216 ; 37896 [ = 0 3 : [ 37896 ; 38577 [ = 0 4 : [ 38577 ; 39257 [ = 1 5 : [ 39257 ; 39938 ] = 1 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 1008 maximum value = 1940 1 : [ 1008 ; 1194 [ = 2 2 : [ 1194 ; 1380 [ = 0 3 : [ 1380 ; 1567 [ = 0 4 : [ 1567 ; 1753 [ = 0 5 : [ 1753 ; 1940 ] = 2 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 1 maximum value = 6 1 : [ 1 ; 2 [ = 6 2 : [ 2 ; 3 [ = 236 3 : [ 3 ; 4 [ = 5006 4 : [ 4 ; 5 [ = 67801 5 : [ 5 ; 6 ] = 2650 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 2 maximum value = 3 1 : [ 2 ; 3 ] = 4 ---------------------------------------------------------- Global definition of the number of elements (cells, vertices, faces...) Synchronizing cell families Renumbering mesh: renumbering for cells: pre-numbering: no renumbering cells adjacent to ghost cells last: no numbering: no renumbering renumbering for interior faces: cell adjacency pre-ordering: lowest id first faces adjacent to ghost cells last: no numbering: multipass renumbering for boundary faces: numbering: no shared cell across threads renumbering for vertices: numbering: no renumbering Numbering for cells: type: default Numbering for interior faces: type: default Numbering for boundary faces: type: default ---------------------------------------------------------- Histogram of volume mesh matrix bandwidth per rank: minimum value = 17488 maximum value = 20153 1 : [ 17488 ; 18021 [ = 1 2 : [ 18021 ; 18554 [ = 0 3 : [ 18554 ; 19087 [ = 0 4 : [ 19087 ; 19620 [ = 1 5 : [ 19620 ; 20153 ] = 2 Histogram of volume mesh matrix profile/lines per rank: minimum value = 7956 maximum value = 10136 1 : [ 7956 ; 8392 [ = 1 2 : [ 8392 ; 8828 [ = 0 3 : [ 8828 ; 9264 [ = 1 4 : [ 9264 ; 9700 [ = 1 5 : [ 9700 ; 10136 ] = 1 Mesh coordinates: minimum and maximum X : -4.8000000e+00 4.8000000e+00 Y : -1.8000000e+00 1.8000000e+00 Z : -3.6739404e-17 2.3000000e+00 Mesh Number of cells: 75699 Number of interior faces: 150675 Number of boundary faces: 5996 Number of vertices: 16253 Groups: "course" cells: 2201 "hexa" cells: 1875 "inlet" boundary faces: 130 "outlet" boundary faces: 143 "wall" boundary faces: 5723 --- Information on the volumes Minimum control volume = 1.6098455e-05 Maximum control volume = 3.8447537e-02 Total volume for the domain = 7.6520000e+01 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 865 --> 1 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 9 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Warning: -------- Mesh quality issue has been detected The mesh should be re-considered using the listed criteria. The calculation will run but the solution quality may be degraded... Computing geometric quantities (0.0636 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 75699 Volume = 7.6520000e+01 Surface = -1 (not computed) Volume zone "all_cells" id = 1 Number of cells = 75699 Volume = 7.6520000e+01 Surface = -1 (not computed) --- Information on boundary zones Boundary zone "boundary_faces" id = 0 Number of faces = 5996 Surface = 1.5016000e+02 Perimeter = -1 (not computed) Boundary zone "BC_1" id = 1 Number of faces = 130 Surface = 1.3000000e+00 Perimeter = -1 (not computed) Boundary zone "BC_2" id = 2 Number of faces = 143 Surface = 1.4300000e+00 Perimeter = -1 (not computed) Boundary zone "BC_3" id = 3 Number of faces = 5723 Surface = 1.4743000e+02 Perimeter = -1 (not computed) ALMAX = 0.42455E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. ------------------------------------------------------------- ----------------------------------------------------------- ** READING MAIN AND AUXILIARY RESTART FILES ---------------------------------------- READING THE MAIN RESTART FILE Start reading Warning: the number of variables or properties has been changed relative to the restart file. current: 5 model and 2 user variables 11 model and 0 user properties previous: 5 model and 0 user variables 11 model and 0 user properties The computation continues, with a partial restart. Reading dimensions complete Reading the previous time step number (restarting computation) NTPABS = 500 Reading the previous time step number (restarting computation) TTPABS = 0.5000E+02 Reading options complete restart/main: section "scalar1::vals::0" not present. restart/main: section "variance1::vals::0" not present. Warning: the following variables could not be found or read in restart file "restart/main", so default initializations will be used: scalar1 variance1 Read variables from restart: restart/main Reading complete READING THE AUXILIARY RESTART FILE Start reading Fin de la lecture des options restart/auxiliary: section "ref_presstot01" not present. @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: WHEN READING THE AUXILIARY RESTART FILE @ ======= @ Lecture des proprietes physiques @ @ It was not possible to read some values from the @ auxiliary restart file. @ They will be initialized by the default values. @ @ This situation can occur when the restart file @ originates from a run realised with different @ options or when the file is damaged. @ @ The run will continue... @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ Fin de la lecture des proprietes physiques Fin de la lecture du pas de temps Fin de la lecture des flux de masse restart/auxiliary: section "scalar1::bc_coeffs::a" not present. restart/auxiliary: section "scalar1::bc_coeffs::b" not present. restart/auxiliary: section "scalar1::bc_coeffs::af" not present. restart/auxiliary: section "scalar1::bc_coeffs::bf" not present. restart/auxiliary: section "variance1::bc_coeffs::a" not present. restart/auxiliary: section "variance1::bc_coeffs::b" not present. restart/auxiliary: section "variance1::bc_coeffs::af" not present. restart/auxiliary: section "variance1::bc_coeffs::bf" not present. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_restart_default.c:2495: Warning Some boundary condition coefficients could not be read from a restart file; they will be initialized with default values. Fin de la lecture des conditions aux limites Fin de la lecture de la distance a la paroi End reading ----------------------------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- Velocity -0.1160E+01 0.9359E+00 Velocity -0.2122E+01 0.7525E+00 Velocity -0.1202E+01 0.7183E+00 Pressure -0.4635E+00 0.1212E+01 k 0.3935E-05 0.9918E-01 omega 0.2449E+00 0.1103E+03 scalar1 0.0000E+00 0.0000E+00 variance1 0.0000E+00 0.0000E+00 Wall distance 0.2547E-02 0.9883E+00 --------------------------------- dt 0.1000E+00 0.1000E+00 --------------------------------- ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 401 40.1 1 500 50 ------------------------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 130 Smooth wall 5 5723 Rough wall 6 0 Symmetry 4 0 Free outlet 3 143 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.501000000E+02 TIME STEP NUMBER 501 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1179E+01 0.1179E+01 molecular_viscos 0.1830E-04 0.1830E-04 turbulent_viscos 0.1208E-04 0.1596E-01 ----------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- scalar1 1 0.2157E-04 0.2157E-04 variance1 2 0.2157E-04 0.2157E-04 ----------------------------------------------- ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.91276E+00 Friction velocity uet : 0.79704E-05 0.10217E+00 Friction velocity uk : 0.82606E-03 0.16064E+00 Dimensionless distance yplus : 0.33582E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.11578E+02 21 0.12481E+00 0.36836E+02 0.10000E+02 c variance1 0.94816E+02 19 0.40629E-01 0.27070E+04 0.10000E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 3.4634e-118 66.028 0.191 0.12584 v variance1 4.1107e-126 463.01 1.2541 1.0129 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.2033 0.8559 -0.1025 m meanVel[Y] -2.318 0.75253 -0.23607 m meanVel[Z] -0.57801 0.74843 -0.017418 m ǁmeanVelǁ 1.985e-05 2.3843 0.43624 m meanPre 0.075718 1.5322 0.50209 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.6031 0.63076 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 402 40.2 1 501 50.1 INSTANT 0.502000000E+02 TIME STEP NUMBER 502 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.15450E+00 0.90909E+00 Friction velocity uet : 0.78467E-05 0.10076E+00 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 1 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.18278E+02 21 0.49520E-01 0.21044E+02 0.43748E+01 c variance1 0.10190E+03 19 0.36163E-01 0.35954E+03 0.29725E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -3.3818 5237 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -1.1946 95.064 0.46403 0.24889 v variance1 0 532.92 2.2383 1.4992 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.2016 0.8559 -0.1024 m meanVel[Y] -2.3128 0.75253 -0.23589 m meanVel[Z] -0.57808 0.74812 -0.017428 m ǁmeanVelǁ 1.985e-05 2.3788 0.43594 m meanPre 0.075541 1.5296 0.50201 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63075 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 403 40.3 1 502 50.2 INSTANT 0.503000000E+02 TIME STEP NUMBER 503 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.45365E+00 0.90890E+00 Friction velocity uet : 0.78468E-05 0.99967E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 2 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.22545E+02 20 0.70181E-01 0.15212E+02 0.27810E+01 c variance1 0.95183E+02 18 0.47739E-01 0.27444E+03 0.25016E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -8.025 5944 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -3.1948 105.27 0.81753 0.37019 v variance1 0 508.77 3.3274 1.8004 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1999 0.8559 -0.1023 m meanVel[Y] -2.3076 0.75253 -0.2357 m meanVel[Z] -0.57815 0.7478 -0.017437 m ǁmeanVelǁ 1.985e-05 2.3733 0.43565 m meanPre 0.075343 1.5271 0.50193 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 404 40.4 1 503 50.3 INSTANT 0.504000000E+02 TIME STEP NUMBER 504 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.49910E+00 0.90889E+00 Friction velocity uet : 0.78468E-05 0.99641E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.25070E+02 20 0.68262E-01 0.12669E+02 0.21041E+01 c variance1 0.90957E+02 18 0.83576E-01 0.23670E+03 0.22717E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -8.1422 6639 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -4.9075 104.33 1.2426 0.49059 v variance1 0 484.52 4.6754 2.0517 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1982 0.8559 -0.10219 m meanVel[Y] -2.3024 0.75253 -0.23552 m meanVel[Z] -0.57822 0.74748 -0.017447 m ǁmeanVelǁ 1.985e-05 2.3679 0.43536 m meanPre 0.075146 1.5245 0.50185 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 405 40.5 1 504 50.4 INSTANT 0.505000000E+02 TIME STEP NUMBER 505 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50122E+00 0.90889E+00 Friction velocity uet : 0.78468E-05 0.99581E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.26778E+02 20 0.53137E-01 0.11424E+02 0.17441E+01 c variance1 0.90762E+02 18 0.83772E-01 0.21167E+03 0.20673E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -14.388 7045 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -9.2472 105.01 1.72 0.61074 v variance1 0 462.63 6.3189 2.3096 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1966 0.8559 -0.10209 m meanVel[Y] -2.2972 0.75253 -0.23533 m meanVel[Z] -0.57829 0.74717 -0.017456 m ǁmeanVelǁ 1.985e-05 2.3625 0.43507 m meanPre 0.07495 1.522 0.50177 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 406 40.6 1 505 50.5 INSTANT 0.506000000E+02 TIME STEP NUMBER 506 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50251E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99539E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.28231E+02 20 0.52490E-01 0.10182E+02 0.14790E+01 c variance1 0.92792E+02 18 0.11451E+00 0.19698E+03 0.18903E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -33.025 7365 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -13.14 104.21 2.2316 0.73079 v variance1 0 459.49 8.239 2.595 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1949 0.8559 -0.10199 m meanVel[Y] -2.2921 0.75253 -0.23515 m meanVel[Z] -0.57836 0.74686 -0.017466 m ǁmeanVelǁ 1.985e-05 2.3571 0.43478 m meanPre 0.074754 1.5195 0.50169 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 407 40.7 1 506 50.6 INSTANT 0.507000000E+02 TIME STEP NUMBER 507 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50328E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99536E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.29428E+02 19 0.48396E-01 0.92983E+01 0.12952E+01 c variance1 0.94774E+02 18 0.10056E+00 0.20055E+03 0.17976E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -44.087 7540 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -17.662 106.28 2.7553 0.85081 v variance1 0 462.3 10.352 2.9132 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1932 0.8559 -0.10189 m meanVel[Y] -2.287 0.75253 -0.23497 m meanVel[Z] -0.57843 0.74655 -0.017475 m ǁmeanVelǁ 1.985e-05 2.3518 0.4345 m meanPre 0.07456 1.517 0.50162 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 408 40.8 1 507 50.7 INSTANT 0.508000000E+02 TIME STEP NUMBER 508 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50373E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99530E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.30467E+02 19 0.49797E-01 0.85259E+01 0.11517E+01 c variance1 0.97239E+02 17 0.10166E+00 0.19794E+03 0.16746E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -52.93 7949 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -21.77 106.11 3.2641 0.97079 v variance1 0 495.87 12.494 3.2629 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1916 0.8559 -0.10179 m meanVel[Y] -2.2819 0.75253 -0.23479 m meanVel[Z] -0.5785 0.74624 -0.017484 m ǁmeanVelǁ 1.985e-05 2.3464 0.43422 m meanPre 0.074367 1.5146 0.50154 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 409 40.9 1 508 50.8 INSTANT 0.509000000E+02 TIME STEP NUMBER 509 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50400E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99530E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.31320E+02 19 0.46866E-01 0.79768E+01 0.10452E+01 c variance1 0.99913E+02 17 0.99057E-01 0.19958E+03 0.15756E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -65.713 7891 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -23.913 103.29 3.7561 1.0907 v variance1 0 632.66 14.549 3.6429 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1899 0.8559 -0.10169 m meanVel[Y] -2.2768 0.75253 -0.23461 m meanVel[Z] -0.57857 0.74593 -0.017494 m ǁmeanVelǁ 1.985e-05 2.3411 0.43395 m meanPre 0.074175 1.5121 0.50146 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 410 41 1 509 50.9 INSTANT 0.510000000E+02 TIME STEP NUMBER 510 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50416E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 510, Physical time 0.51000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 510: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.32054E+02 18 0.40947E-01 0.74432E+01 0.95458E+00 c variance1 0.10304E+03 17 0.94617E-01 0.19876E+03 0.14734E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -62.319 8112 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -24.899 106.78 4.2107 1.2107 v variance1 0 708.44 16.46 4.0486 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1883 0.8559 -0.10159 m meanVel[Y] -2.2718 0.75253 -0.23443 m meanVel[Z] -0.57864 0.74562 -0.017503 m ǁmeanVelǁ 1.985e-05 2.3359 0.43367 m meanPre 0.073983 1.5096 0.50138 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 411 41.1 1 510 51 INSTANT 0.511000000E+02 TIME STEP NUMBER 511 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50424E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99530E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.32731E+02 18 0.39053E-01 0.69752E+01 0.87909E+00 c variance1 0.10669E+03 17 0.95670E-01 0.19485E+03 0.13699E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -70.081 8150 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -23.016 110.13 4.6258 1.3306 v variance1 0 766.37 18.154 4.4782 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1867 0.8559 -0.10149 m meanVel[Y] -2.2668 0.75253 -0.23425 m meanVel[Z] -0.5787 0.74532 -0.017512 m ǁmeanVelǁ 1.985e-05 2.3306 0.4334 m meanPre 0.073742 1.5072 0.5013 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 412 41.2 1 511 51.1 INSTANT 0.512000000E+02 TIME STEP NUMBER 512 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50430E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.33399E+02 18 0.41124E-01 0.65274E+01 0.81275E+00 c variance1 0.11070E+03 17 0.94130E-01 0.19086E+03 0.12774E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -73.929 8285 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -21.578 106.89 4.9997 1.4506 v variance1 0 777.09 19.649 4.928 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1851 0.8559 -0.10139 m meanVel[Y] -2.2618 0.75253 -0.23407 m meanVel[Z] -0.57877 0.74501 -0.017521 m ǁmeanVelǁ 1.985e-05 2.3254 0.43313 m meanPre 0.073486 1.5048 0.50123 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 413 41.3 1 512 51.2 INSTANT 0.513000000E+02 TIME STEP NUMBER 513 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50433E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.34070E+02 17 0.39728E-01 0.61755E+01 0.75876E+00 c variance1 0.11565E+03 17 0.91021E-01 0.18418E+03 0.11842E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -78.759 8290 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -24.188 107.98 5.3345 1.5705 v variance1 0 800.41 20.956 5.3971 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1835 0.8559 -0.10129 m meanVel[Y] -2.2568 0.75253 -0.23389 m meanVel[Z] -0.57884 0.74471 -0.01753 m ǁmeanVelǁ 1.985e-05 2.3202 0.43287 m meanPre 0.073232 1.5024 0.50115 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 414 41.4 1 513 51.3 INSTANT 0.514000000E+02 TIME STEP NUMBER 514 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50434E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.34812E+02 17 0.39984E-01 0.58756E+01 0.71227E+00 c variance1 0.12081E+03 17 0.87076E-01 0.17764E+03 0.11021E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -81.775 8320 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -27.8 109.07 5.632 1.6905 v variance1 0 824.69 22.136 5.8802 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1819 0.8559 -0.10119 m meanVel[Y] -2.2519 0.75253 -0.23372 m meanVel[Z] -0.57891 0.74441 -0.017539 m ǁmeanVelǁ 1.985e-05 2.315 0.4326 m meanPre 0.072979 1.5 0.50108 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 415 41.5 1 514 51.4 INSTANT 0.515000000E+02 TIME STEP NUMBER 515 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50435E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.35523E+02 17 0.37450E-01 0.56659E+01 0.67548E+00 c variance1 0.12673E+03 17 0.89279E-01 0.17305E+03 0.10325E+01 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -78.798 8257 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -22.842 109.25 5.9 1.8104 v variance1 0 835.52 23.212 6.3803 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1803 0.8559 -0.1011 m meanVel[Y] -2.2469 0.75253 -0.23354 m meanVel[Z] -0.57897 0.74411 -0.017548 m ǁmeanVelǁ 1.985e-05 2.3099 0.43234 m meanPre 0.072727 1.4976 0.501 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 416 41.6 1 515 51.5 INSTANT 0.516000000E+02 TIME STEP NUMBER 516 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50436E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.36324E+02 16 0.35811E-01 0.53644E+01 0.63611E+00 c variance1 0.13256E+03 17 0.91779E-01 0.17040E+03 0.97681E+00 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -78.953 8369 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -25.935 108.84 6.14 1.9304 v variance1 0 890.36 24.2 6.8898 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1787 0.8559 -0.101 m meanVel[Y] -2.242 0.75253 -0.23337 m meanVel[Z] -0.57904 0.74381 -0.017557 m ǁmeanVelǁ 1.985e-05 2.3048 0.43208 m meanPre 0.072476 1.4952 0.50092 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 417 41.7 1 516 51.6 INSTANT 0.517000000E+02 TIME STEP NUMBER 517 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50436E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.37147E+02 17 0.37341E-01 0.51655E+01 0.60545E+00 c variance1 0.13828E+03 16 0.90296E-01 0.16642E+03 0.92361E+00 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -82.547 8294 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -22.048 110.11 6.362 2.0503 v variance1 0 868.59 25.113 7.4079 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1771 0.8559 -0.1009 m meanVel[Y] -2.2372 0.75253 -0.23319 m meanVel[Z] -0.57911 0.74352 -0.017566 m ǁmeanVelǁ 1.985e-05 2.2997 0.43183 m meanPre 0.072227 1.4928 0.50085 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 418 41.8 1 517 51.7 INSTANT 0.518000000E+02 TIME STEP NUMBER 518 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50436E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.37982E+02 16 0.36046E-01 0.49747E+01 0.57747E+00 c variance1 0.14447E+03 16 0.83977E-01 0.16537E+03 0.88223E+00 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -80.353 8356 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -20.141 110.82 6.5631 2.1703 v variance1 0 944.32 26.002 7.9358 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1755 0.8559 -0.10081 m meanVel[Y] -2.2323 0.75253 -0.23302 m meanVel[Z] -0.57917 0.74322 -0.017575 m ǁmeanVelǁ 1.985e-05 2.2946 0.43158 m meanPre 0.071979 1.4904 0.50077 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 419 41.9 1 518 51.8 INSTANT 0.519000000E+02 TIME STEP NUMBER 519 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50437E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.38856E+02 16 0.36226E-01 0.47751E+01 0.55074E+00 c variance1 0.15091E+03 16 0.91803E-01 0.16320E+03 0.84188E+00 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -85.494 8200 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -21.963 112.72 6.7476 2.2902 v variance1 0 911.38 26.845 8.4681 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.174 0.8559 -0.10071 m meanVel[Y] -2.2275 0.75253 -0.23285 m meanVel[Z] -0.57924 0.74293 -0.017584 m ǁmeanVelǁ 1.985e-05 2.2896 0.43133 m meanPre 0.071732 1.4881 0.5007 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 420 42 1 519 51.9 INSTANT 0.520000000E+02 TIME STEP NUMBER 520 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 130 -0.107429594E+01 Smooth wall 5 5723 0.267105663E-29 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 143 0.107429594E+01 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.50437E+00 0.90888E+00 Friction velocity uet : 0.78468E-05 0.99529E-01 Friction velocity uk : 0.82574E-03 0.16064E+00 Dimensionless distance yplus : 0.33577E+01 0.51184E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 357 Total number of wall faces : 5723 ------------------------------------------------------------ Write final restart files checkpoint at iteration 520, Physical time 0.52000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 520: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c scalar1 0.39748E+02 17 0.36498E-01 0.46341E+01 0.52895E+00 c variance1 0.15688E+03 17 0.89571E-01 0.16509E+03 0.81578E+00 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------- -------------- -------------- ------------ ------------ a scalar1 a variance1 -75.806 8280 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1598 0.93589 -0.060649 -0.02006 v Velocity[Y] -2.1218 0.75253 -0.16082 -0.047742 v Velocity[Z] -1.2018 0.71831 -0.021278 0.0014246 v ǁVelocityǁ 1.985e-05 2.1729 0.41088 0.23406 v Pressure -0.46351 1.212 0.46956 0.47132 v scalar1 -23.58 114.68 6.9214 2.4101 v variance1 0 875.44 27.628 9.0045 v Wall distance 0.002547 0.98826 0.35336 0.3355 m meanVel[X] -1.1724 0.8559 -0.10062 m meanVel[Y] -2.2227 0.75253 -0.23268 m meanVel[Z] -0.5793 0.74264 -0.017592 m ǁmeanVelǁ 1.985e-05 2.2846 0.43108 m meanPre 0.071486 1.4858 0.50063 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.00026905 17.188 1.603 0.63074 ** Temporal moment accumulated weights ----------------------------------- id n it. value ---- -------- -------------- 0 421 42.1 1 520 52 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation