command: ./cs_solver --trace --mpi *************************************************************** (R) Code_Saturne Version 7.0.2 Copyright (C) 1998-2021 EDF S.A., France revision d029e16a2 build Thu 30 Jun 2022 03:27:14 PM MSK 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: Mon 24 Oct 2022 11:29:00 AM MSK System: Linux 3.10.0-1160.66.1.el7.x86_64 Machine: XeonLinux Processor: model name : Intel(R) Xeon(R) CPU E5-2678 v3 @ 2.50GHz Memory: 64331 MB User: antech (Andrew) Directory: /run/media/antech/HDD Data/Storage/Media/Work/Svetly/DustLine/Saturne/RESU/20221024-1128 MPI ranks: 4 (appnum attribute: 0) OpenMP threads: 1 Processors/node: 1 Compilers used for build: C compiler: gcc (GCC) 4.8.5 20150623 (Red Hat 4.8.5-44) C++ compiler: g++ (GCC) 4.8.5 20150623 (Red Hat 4.8.5-44) Fortran compiler: GNU Fortran (GCC) 4.8.5 20150623 (Red Hat 4.8.5-44) MPI version 3.0 (Open MPI 1.8.4) 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: SCOTCH 5.1.12 =============================================================== 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 = 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 ------------- --- 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 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 ) 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 = 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 = 208 (Initial time step) NTMABS = 10000000 (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 = 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) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: separate_meshes time dependency: fixed mesh output: at end -5: name: directory: monitoring format: time_plot options: CSV time dependency: fixed mesh output: every time step -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at end Code_Saturne: ../../../source/src/mesh/cs_partition.c:2910: Warning Partitioning with LibSCOTCH requested, but PT-SCOTCH is not available, so serial SCOTCH will be used. Reading file: restart/mesh_input.csm Finished reading: restart/mesh_input.csm No "partition_input/domain_number_4" file available; ---------------------------------------------------------- Partitioning 6236725 cells to 4 domains (SCOTCH_graphPart). Total number of faces on parallel boundaries: 4619 wall-clock time: 6.994282 s Number of cells per domain (histogramm): [ 1481440 ; 1496965 [ = 2 [ 1496965 ; 1512490 [ = 0 [ 1512490 ; 1528015 [ = 0 [ 1528015 ; 1543540 [ = 0 [ 1543540 ; 1559065 [ = 0 [ 1559065 ; 1574590 [ = 0 [ 1574590 ; 1590115 [ = 0 [ 1590115 ; 1605640 [ = 0 [ 1605640 ; 1621165 [ = 0 [ 1621165 ; 1636690 ] = 2 Writing file: partition_output/domain_number_4 Finished writing: partition_output/domain_number_4 Partitioning finished (8.55 s) ---------------------------------------------------------- Halo construction with extended neighborhood ============================================ Face interfaces creation Vertex interfaces creation Halo creation Halo definition Local halo definition Distant halo creation Updating the faces -> cells connectivity Extended neighborhood structures definition Histogram of the number of cells per rank: minimum value = 1481440 maximum value = 1636690 1 : [ 1481440 ; 1512490 [ = 2 2 : [ 1512490 ; 1543540 [ = 0 3 : [ 1543540 ; 1574590 [ = 0 4 : [ 1574590 ; 1605640 [ = 0 5 : [ 1605640 ; 1636690 ] = 2 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 1484913 maximum value = 1642952 1 : [ 1484913 ; 1516520 [ = 2 2 : [ 1516520 ; 1548128 [ = 0 3 : [ 1548128 ; 1579736 [ = 0 4 : [ 1579736 ; 1611344 [ = 0 5 : [ 1611344 ; 1642952 ] = 2 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 3267 maximum value = 6441 1 : [ 3267 ; 3901 [ = 2 2 : [ 3901 ; 4536 [ = 0 3 : [ 4536 ; 5171 [ = 0 4 : [ 5171 ; 5806 [ = 0 5 : [ 5806 ; 6441 ] = 2 Histogram of the number of ghost cells in the standard neighborhood per rank: minimum value = 1541 maximum value = 2996 1 : [ 1541 ; 1832 [ = 2 2 : [ 1832 ; 2123 [ = 0 3 : [ 2123 ; 2414 [ = 0 4 : [ 2414 ; 2705 [ = 0 5 : [ 2705 ; 2996 ] = 2 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 3576541 maximum value = 3953593 1 : [ 3576541 ; 3651951 [ = 2 2 : [ 3651951 ; 3727361 [ = 0 3 : [ 3727361 ; 3802772 [ = 0 4 : [ 3802772 ; 3878182 [ = 0 5 : [ 3878182 ; 3953593 ] = 2 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 45557 maximum value = 51538 1 : [ 45557 ; 46753 [ = 1 2 : [ 46753 ; 47949 [ = 1 3 : [ 47949 ; 49145 [ = 0 4 : [ 49145 ; 50341 [ = 1 5 : [ 50341 ; 51538 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 3 maximum value = 5 1 : [ 3 ; 4 [ = 318 2 : [ 4 ; 5 ] = 6236407 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 1 maximum value = 2 1 : [ 1 ; 2 ] = 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 = 1481474 maximum value = 1635755 1 : [ 1481474 ; 1512330 [ = 2 2 : [ 1512330 ; 1543186 [ = 0 3 : [ 1543186 ; 1574042 [ = 0 4 : [ 1574042 ; 1604898 [ = 0 5 : [ 1604898 ; 1635755 ] = 2 Histogram of volume mesh matrix profile/lines per rank: minimum value = 130345 maximum value = 143534 1 : [ 130345 ; 132982 [ = 2 2 : [ 132982 ; 135620 [ = 0 3 : [ 135620 ; 138258 [ = 0 4 : [ 138258 ; 140896 [ = 0 5 : [ 140896 ; 143534 ] = 2 Mesh coordinates: minimum and maximum X : -8.7784996e+00 1.0360302e+01 Y : 8.1000004e+00 1.2088500e+01 Z : -6.4325452e+00 1.3896698e+01 Mesh Number of cells: 6236725 Number of interior faces: 15056921 Number of boundary faces: 194218 Number of vertices: 2876943 Groups: "INLET" boundary faces: 1365 "OUTLET" boundary faces: 1383 "VOLUME" cells: 6236725 "WALL" boundary faces: 191470 --- Information on the volumes Minimum control volume = 5.5486462e-09 Maximum control volume = 4.8423066e-06 Total volume for the domain = 4.4578971e+00 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 30774 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 598 --> 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 (2.55 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 6236725 Volume = 4.4579 Center of gravity = (-2.5753, 11.547, 5.4877) Surface = -1 (not computed) Volume zone "all_cells" id = 1 Number of cells = 6236725 Volume = 4.4579 Center of gravity = (-2.5753, 11.547, 5.4877) Surface = -1 (not computed) --- Information on boundary zones Boundary zone "boundary_faces" id = 0 Number of faces = 194218 Surface = 50.239 Center of gravity = (-2.5514, 11.538, 5.4884) Perimeter = -1 (not computed) Boundary zone "INLET" id = 1 Number of faces = 1365 Surface = 0.099773 Center of gravity = (10.182, 8.1, 13.718) Perimeter = -1 (not computed) Boundary zone "OUTLET" id = 2 Number of faces = 1383 Surface = 0.099773 Center of gravity = (-3.2547, 10.69, -2.3561) Perimeter = -1 (not computed) Boundary zone "WALL" id = 3 Number of faces = 191470 Surface = 50.04 Center of gravity = (-2.5754, 11.547, 5.4876) Perimeter = -1 (not computed) ALMAX = 0.16458E+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 Reading dimensions complete Reading the previous time step number (restarting computation) NTPABS = 208 Reading the previous time step number (restarting computation) TTPABS = 0.2080E-02 Reading options complete Read variables from restart: restart/main.csc Reading complete READING THE AUXILIARY RESTART FILE Start reading Finished reading options restart/auxiliary.csc: 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 Fin de la lecture des conditions aux limites Fin de la lecture des termes sources restart/auxiliary.csc: section "time_moments:sizes" not present. Fin de la lecture de la distance a la paroi End reading ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.8080E+00 0.8080E+00 molecular_viscos 0.2150E-04 0.2150E-04 turbulent_viscos 0.8459E-07 0.1056E-01 ----------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 1365 Smooth wall 5 0 Rough wall 6 191470 Symmetry 4 0 Free outlet 3 1383 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.129 26.251 -4.4426 -6.0615 v Velocity[Y] -23.644 27.337 0.85814 1.1685 v Velocity[Z] -27.315 18.181 -5.3418 -7.2517 v ǁVelocityǁ 0.0086547 29.475 15.108 20.132 v Pressure -306.43 449.83 186.35 186.14 v k 0.0057891 9.6424 1.0259 0.6805 v omega 106.25 6.8747e+05 11431 718.31 v TurbVisc 8.4591e-08 0.010556 0.00080794 0.0010439 v CourantNb 0 0 0 0 v FourierNb 0 0 0 0 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1459e-05 0.01 0.00062542 0.00049096 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0 0 0 =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.209000000E-02 TIME STEP NUMBER 209 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499839E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58295E-01 0.35819E+02 Friction velocity uk : 0.41674E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10691E+03 6 0.45272E-03 0.70995E+00 0.19955E+01 c Velocity[X] 0.27796E+00 c Velocity[Y] 0.15091E+00 c Velocity[Z] 0.28108E+00 c Pressure 0.80904E-03 10 0.56633E-04 0.11428E-01 0.43504E+00 c k 0.31090E+01 6 0.24780E-05 0.56142E-01 0.10265E+02 c omega 0.26938E+05 3 0.11929E-05 0.21190E+05 0.11481E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.126 26.251 -4.4426 -6.0615 v Velocity[Y] -23.646 27.33 0.85815 1.1685 v Velocity[Z] -27.31 18.224 -5.3419 -7.2517 v ǁVelocityǁ 0.0094048 29.447 15.109 20.132 v Pressure -306.42 449.8 186.36 186.14 v k 0.0058336 9.6266 1.0258 0.68117 v omega 105.98 6.8747e+05 11432 717.7 v TurbVisc 8.4591e-08 0.010556 0.00080794 0.0010439 v CourantNb 0.0031132 1.0596 0.9396 0.99859 v FourierNb 0.0050509 10 2.8396 0.32585 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1456e-05 0.01 0.00062537 0.00049095 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99825 11.024 3.7792 1.3244 INSTANT 0.210000000E-02 TIME STEP NUMBER 210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499928E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62374E-01 0.35898E+02 Friction velocity uk : 0.41834E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10692E+03 6 0.45482E-03 0.70779E+00 0.19967E+01 c Velocity[X] 0.27778E+00 c Velocity[Y] 0.15019E+00 c Velocity[Z] 0.27982E+00 c Pressure 0.81660E-03 11 0.57580E-04 0.11535E-01 0.42634E+00 c k 0.31132E+01 6 0.24562E-05 0.55403E-01 0.10204E+02 c omega 0.26941E+05 3 0.11726E-05 0.20863E+05 0.11380E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.156 26.251 -4.4426 -6.0615 v Velocity[Y] -23.636 27.324 0.85816 1.1685 v Velocity[Z] -27.3 18.262 -5.3421 -7.2517 v ǁVelocityǁ 0.012798 29.469 15.11 20.132 v Pressure -306.08 449.76 186.36 186.14 v k 0.0058774 9.6159 1.0258 0.68185 v omega 105.7 6.8747e+05 11432 717.1 v TurbVisc 8.4684e-08 0.010556 0.00080969 0.0010476 v CourantNb 0.0029966 1.0875 0.9396 0.99859 v FourierNb 0.0050625 10 2.8384 0.32576 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1452e-05 0.01 0.00062532 0.00049094 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99838 11.033 3.778 1.3244 INSTANT 0.211000000E-02 TIME STEP NUMBER 211 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500006E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86837E-01 0.35782E+02 Friction velocity uk : 0.41991E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10692E+03 6 0.44409E-03 0.70305E+00 0.19896E+01 c Velocity[X] 0.27577E+00 c Velocity[Y] 0.14929E+00 c Velocity[Z] 0.27799E+00 c Pressure 0.82489E-03 13 0.60116E-04 0.11652E-01 0.54413E+00 c k 0.31174E+01 6 0.24414E-05 0.54677E-01 0.10142E+02 c omega 0.26944E+05 3 0.11611E-05 0.20625E+05 0.11304E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.127 26.253 -4.4426 -6.0615 v Velocity[Y] -23.64 27.317 0.85817 1.1685 v Velocity[Z] -27.295 18.295 -5.3422 -7.2517 v ǁVelocityǁ 0.012792 29.475 15.111 20.132 v Pressure -306.27 449.56 186.37 186.15 v k 0.0059212 9.5945 1.0257 0.68253 v omega 105.44 6.8747e+05 11432 716.51 v TurbVisc 8.4749e-08 0.010556 0.00081143 0.0010513 v CourantNb 0.0030345 1.0437 0.9396 0.99859 v FourierNb 0.0050741 10 2.8372 0.32568 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1448e-05 0.01 0.00062527 0.00049093 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99884 11.017 3.7768 1.3243 INSTANT 0.212000000E-02 TIME STEP NUMBER 212 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500056E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86058E-01 0.35836E+02 Friction velocity uk : 0.42147E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10693E+03 6 0.45134E-03 0.69819E+00 0.19858E+01 c Velocity[X] 0.27467E+00 c Velocity[Y] 0.14783E+00 c Velocity[Z] 0.27568E+00 c Pressure 0.81896E-03 13 0.57415E-04 0.11568E-01 0.55924E+00 c k 0.31216E+01 6 0.24170E-05 0.53961E-01 0.10081E+02 c omega 0.26948E+05 3 0.11465E-05 0.20306E+05 0.11209E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.11 26.258 -4.4425 -6.0615 v Velocity[Y] -23.646 27.31 0.85819 1.1685 v Velocity[Z] -27.291 18.339 -5.3423 -7.2517 v ǁVelocityǁ 0.015643 29.472 15.112 20.132 v Pressure -306.26 449.42 186.39 186.17 v k 0.0059645 9.5772 1.0257 0.68321 v omega 105.19 6.8747e+05 11433 715.93 v TurbVisc 8.4821e-08 0.010556 0.00081317 0.0010551 v CourantNb 0.0030192 1.118 0.9396 0.99859 v FourierNb 0.0050856 10 2.836 0.32561 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1444e-05 0.01 0.00062522 0.00049092 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99833 11.034 3.7756 1.3242 INSTANT 0.213000000E-02 TIME STEP NUMBER 213 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500081E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10751E+00 0.35793E+02 Friction velocity uk : 0.42301E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10694E+03 6 0.45752E-03 0.69474E+00 0.19803E+01 c Velocity[X] 0.27355E+00 c Velocity[Y] 0.14688E+00 c Velocity[Z] 0.27431E+00 c Pressure 0.83086E-03 13 0.58411E-04 0.11736E-01 0.54937E+00 c k 0.31258E+01 6 0.24047E-05 0.53267E-01 0.10021E+02 c omega 0.26951E+05 3 0.11470E-05 0.20158E+05 0.11149E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.119 26.264 -4.4425 -6.0615 v Velocity[Y] -23.655 27.304 0.8582 1.1685 v Velocity[Z] -27.279 18.412 -5.3424 -7.2517 v ǁVelocityǁ 0.015129 29.464 15.113 20.132 v Pressure -306.4 449.49 186.4 186.18 v k 0.0060065 9.5668 1.0256 0.6839 v omega 104.96 6.8747e+05 11433 715.35 v TurbVisc 8.4887e-08 0.010556 0.00081492 0.0010588 v CourantNb 0.0030382 1.0437 0.9396 0.99859 v FourierNb 0.005097 10 2.8349 0.32554 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.144e-05 0.01 0.00062518 0.0004909 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99901 11.033 3.7745 1.3241 INSTANT 0.214000000E-02 TIME STEP NUMBER 214 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500100E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19349E-01 0.35815E+02 Friction velocity uk : 0.42449E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10695E+03 6 0.44340E-03 0.69028E+00 0.19785E+01 c Velocity[X] 0.27212E+00 c Velocity[Y] 0.14551E+00 c Velocity[Z] 0.27264E+00 c Pressure 0.81981E-03 13 0.56039E-04 0.11580E-01 0.71692E+00 c k 0.31299E+01 6 0.23836E-05 0.52585E-01 0.99611E+01 c omega 0.26955E+05 3 0.11301E-05 0.20034E+05 0.11095E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.094 26.266 -4.4424 -6.0615 v Velocity[Y] -23.662 27.297 0.85821 1.1685 v Velocity[Z] -27.272 18.488 -5.3425 -7.2517 v ǁVelocityǁ 0.015999 29.44 15.114 20.133 v Pressure -307.1 449.3 186.43 186.2 v k 0.006045 9.5512 1.0256 0.68458 v omega 104.7 6.8747e+05 11434 714.79 v TurbVisc 8.4942e-08 0.010556 0.00081666 0.0010625 v CourantNb 0.0029047 1.0492 0.9396 0.99859 v FourierNb 0.0051084 10 2.8338 0.32547 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1437e-05 0.01 0.00062513 0.00049089 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99906 11.032 3.7734 1.3241 INSTANT 0.215000000E-02 TIME STEP NUMBER 215 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500113E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83775E-01 0.35919E+02 Friction velocity uk : 0.42585E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10696E+03 6 0.45090E-03 0.68466E+00 0.19698E+01 c Velocity[X] 0.27045E+00 c Velocity[Y] 0.14421E+00 c Velocity[Z] 0.27000E+00 c Pressure 0.80737E-03 13 0.57548E-04 0.11404E-01 0.47071E+00 c k 0.31341E+01 6 0.23471E-05 0.51921E-01 0.99026E+01 c omega 0.26958E+05 3 0.11118E-05 0.19715E+05 0.11006E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.09 26.269 -4.4424 -6.0615 v Velocity[Y] -23.658 27.289 0.85823 1.1685 v Velocity[Z] -27.268 18.562 -5.3427 -7.2517 v ǁVelocityǁ 0.015927 29.444 15.115 20.133 v Pressure -306.76 449.3 186.42 186.2 v k 0.0060842 9.5396 1.0256 0.68528 v omega 104.44 6.8747e+05 11434 714.23 v TurbVisc 8.4954e-08 0.010556 0.0008184 0.0010662 v CourantNb 0.0031304 1.0529 0.9396 0.99859 v FourierNb 0.0051196 10 2.8327 0.32541 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1431e-05 0.01 0.00062508 0.00049088 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99956 11.018 3.7723 1.324 INSTANT 0.216000000E-02 TIME STEP NUMBER 216 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500120E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10781E+00 0.35880E+02 Friction velocity uk : 0.42723E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10696E+03 6 0.45833E-03 0.68214E+00 0.19692E+01 c Velocity[X] 0.26950E+00 c Velocity[Y] 0.14322E+00 c Velocity[Z] 0.26942E+00 c Pressure 0.82669E-03 13 0.54448E-04 0.11677E-01 0.56900E+00 c k 0.31383E+01 6 0.23123E-05 0.51261E-01 0.98437E+01 c omega 0.26962E+05 3 0.11038E-05 0.19460E+05 0.10927E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.115 26.268 -4.4424 -6.0615 v Velocity[Y] -23.665 27.283 0.85824 1.1685 v Velocity[Z] -27.257 18.637 -5.3428 -7.2517 v ǁVelocityǁ 0.015515 29.449 15.116 20.133 v Pressure -306.59 449.04 186.41 186.19 v k 0.0061205 9.5324 1.0255 0.68597 v omega 104.19 6.8747e+05 11435 713.68 v TurbVisc 8.4873e-08 0.010556 0.00082014 0.00107 v CourantNb 0.0028633 1.0601 0.9396 0.99859 v FourierNb 0.0051309 10 2.8316 0.32536 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1428e-05 0.01 0.00062504 0.00049087 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0002 11.024 3.7712 1.3239 INSTANT 0.217000000E-02 TIME STEP NUMBER 217 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500125E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62199E-01 0.35813E+02 Friction velocity uk : 0.42850E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10697E+03 6 0.45635E-03 0.67686E+00 0.19631E+01 c Velocity[X] 0.26793E+00 c Velocity[Y] 0.14159E+00 c Velocity[Z] 0.26734E+00 c Pressure 0.82091E-03 13 0.57500E-04 0.11595E-01 0.45197E+00 c k 0.31425E+01 6 0.22764E-05 0.50615E-01 0.97852E+01 c omega 0.26966E+05 3 0.10829E-05 0.19140E+05 0.10827E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.082 26.268 -4.4423 -6.0615 v Velocity[Y] -23.678 27.277 0.85826 1.1685 v Velocity[Z] -27.253 18.71 -5.3429 -7.2517 v ǁVelocityǁ 0.015204 29.458 15.117 20.133 v Pressure -307.09 448.96 186.4 186.18 v k 0.0061593 9.5244 1.0255 0.68667 v omega 103.96 6.8747e+05 11435 713.14 v TurbVisc 8.4834e-08 0.010556 0.00082188 0.0010737 v CourantNb 0.0030215 1.0401 0.9396 0.99859 v FourierNb 0.005142 10 2.8306 0.3253 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1425e-05 0.01 0.00062499 0.00049086 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0001 11.014 3.7702 1.3239 INSTANT 0.218000000E-02 TIME STEP NUMBER 218 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500137E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10550E+00 0.35949E+02 Friction velocity uk : 0.42986E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10698E+03 6 0.45692E-03 0.67212E+00 0.19578E+01 c Velocity[X] 0.26639E+00 c Velocity[Y] 0.14037E+00 c Velocity[Z] 0.26537E+00 c Pressure 0.81859E-03 10 0.53608E-04 0.11563E-01 0.43287E+00 c k 0.31466E+01 6 0.22524E-05 0.49981E-01 0.97278E+01 c omega 0.26970E+05 3 0.10724E-05 0.18858E+05 0.10739E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.067 26.269 -4.4423 -6.0615 v Velocity[Y] -23.678 27.269 0.85828 1.1685 v Velocity[Z] -27.249 18.782 -5.343 -7.2517 v ǁVelocityǁ 0.015889 29.455 15.118 20.133 v Pressure -307 448.84 186.39 186.17 v k 0.006191 9.5199 1.0256 0.68737 v omega 103.72 6.8747e+05 11436 712.61 v TurbVisc 8.4767e-08 0.010556 0.00082362 0.0010774 v CourantNb 0.0029378 1.0479 0.9396 0.99859 v FourierNb 0.0051531 10 2.8296 0.32526 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1421e-05 0.01 0.00062495 0.00049085 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0001 11.048 3.7692 1.3238 INSTANT 0.219000000E-02 TIME STEP NUMBER 219 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500159E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10796E+00 0.35900E+02 Friction velocity uk : 0.43096E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10699E+03 6 0.45721E-03 0.66802E+00 0.19534E+01 c Velocity[X] 0.26502E+00 c Velocity[Y] 0.13890E+00 c Velocity[Z] 0.26411E+00 c Pressure 0.82886E-03 12 0.55679E-04 0.11708E-01 0.44228E+00 c k 0.31508E+01 6 0.22256E-05 0.49358E-01 0.96706E+01 c omega 0.26973E+05 3 0.10714E-05 0.18762E+05 0.10699E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.07 26.264 -4.4422 -6.0615 v Velocity[Y] -23.695 27.263 0.8583 1.1685 v Velocity[Z] -27.237 18.852 -5.3431 -7.2517 v ǁVelocityǁ 0.016454 29.439 15.119 20.133 v Pressure -307.22 448.82 186.38 186.15 v k 0.0062196 9.5167 1.0256 0.68807 v omega 103.49 6.8747e+05 11436 712.08 v TurbVisc 8.4741e-08 0.010556 0.00082537 0.0010811 v CourantNb 0.0028959 1.0459 0.9396 0.99859 v FourierNb 0.0051641 10 2.8287 0.32522 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1417e-05 0.01 0.0006249 0.00049084 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0001 11.02 3.7683 1.3238 INSTANT 0.220000000E-02 TIME STEP NUMBER 220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500181E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11401E+00 0.35794E+02 Friction velocity uk : 0.43196E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10699E+03 6 0.45537E-03 0.66321E+00 0.19482E+01 c Velocity[X] 0.26353E+00 c Velocity[Y] 0.13739E+00 c Velocity[Z] 0.26229E+00 c Pressure 0.83582E-03 13 0.51898E-04 0.11806E-01 0.88624E+00 c k 0.31549E+01 6 0.22113E-05 0.48737E-01 0.96132E+01 c omega 0.26977E+05 3 0.10625E-05 0.18668E+05 0.10651E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.055 26.258 -4.4422 -6.0615 v Velocity[Y] -23.713 27.256 0.85832 1.1685 v Velocity[Z] -27.231 18.923 -5.3432 -7.2517 v ǁVelocityǁ 0.016085 29.452 15.12 20.133 v Pressure -308.12 448.31 186.32 186.09 v k 0.0062498 9.5106 1.0256 0.68878 v omega 103.27 6.8747e+05 11437 711.56 v TurbVisc 8.4664e-08 0.010556 0.00082711 0.0010848 v CourantNb 0.0028145 1.0693 0.9396 0.99859 v FourierNb 0.0051751 10 2.8277 0.32518 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1413e-05 0.01 0.00062486 0.00049083 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0002 11.028 3.7673 1.3238 INSTANT 0.221000000E-02 TIME STEP NUMBER 221 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500204E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70775E-01 0.35897E+02 Friction velocity uk : 0.43300E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10700E+03 6 0.45541E-03 0.65856E+00 0.19430E+01 c Velocity[X] 0.26199E+00 c Velocity[Y] 0.13622E+00 c Velocity[Z] 0.26036E+00 c Pressure 0.81407E-03 13 0.54401E-04 0.11499E-01 0.83205E+00 c k 0.31591E+01 6 0.21694E-05 0.48138E-01 0.95573E+01 c omega 0.26981E+05 3 0.10442E-05 0.18371E+05 0.10558E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.077 26.248 -4.4421 -6.0615 v Velocity[Y] -23.728 27.249 0.85834 1.1685 v Velocity[Z] -27.227 18.992 -5.3433 -7.2517 v ǁVelocityǁ 0.014791 29.464 15.121 20.133 v Pressure -307.91 448.3 186.26 186.04 v k 0.0062762 9.5069 1.0256 0.68949 v omega 103.05 6.8747e+05 11437 711.05 v TurbVisc 8.463e-08 0.010556 0.00082885 0.0010885 v CourantNb 0.0030865 1.0395 0.9396 0.99859 v FourierNb 0.005186 10 2.8268 0.32514 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.141e-05 0.01 0.00062482 0.00049082 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99943 11.015 3.7664 1.3237 INSTANT 0.222000000E-02 TIME STEP NUMBER 222 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500228E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49363E-01 0.35802E+02 Friction velocity uk : 0.43392E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10701E+03 6 0.45989E-03 0.65324E+00 0.19364E+01 c Velocity[X] 0.26031E+00 c Velocity[Y] 0.13443E+00 c Velocity[Z] 0.25850E+00 c Pressure 0.81504E-03 13 0.52928E-04 0.11512E-01 0.10591E+01 c k 0.31632E+01 6 0.21447E-05 0.47546E-01 0.95019E+01 c omega 0.26985E+05 3 0.10373E-05 0.18116E+05 0.10482E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.048 26.238 -4.4421 -6.0615 v Velocity[Y] -23.744 27.242 0.85836 1.1685 v Velocity[Z] -27.217 19.061 -5.3434 -7.2517 v ǁVelocityǁ 0.015707 29.481 15.121 20.133 v Pressure -307.69 448.16 186.19 185.96 v k 0.0062978 9.5019 1.0257 0.6902 v omega 102.77 6.8747e+05 11438 710.55 v TurbVisc 8.4575e-08 0.010556 0.00083059 0.0010922 v CourantNb 0.002787 1.0321 0.9396 0.99859 v FourierNb 0.0051969 10 2.8259 0.32511 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1406e-05 0.01 0.00062477 0.00049081 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0007 11.01 3.7655 1.3237 INSTANT 0.223000000E-02 TIME STEP NUMBER 223 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500243E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27739E-01 0.35919E+02 Friction velocity uk : 0.43467E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10702E+03 6 0.46552E-03 0.64863E+00 0.19310E+01 c Velocity[X] 0.25846E+00 c Velocity[Y] 0.13294E+00 c Velocity[Z] 0.25723E+00 c Pressure 0.82247E-03 22 0.52934E-04 0.11617E-01 0.96439E+01 c k 0.31674E+01 6 0.20994E-05 0.46963E-01 0.94468E+01 c omega 0.26989E+05 3 0.10292E-05 0.18086E+05 0.10454E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.051 26.23 -4.442 -6.0615 v Velocity[Y] -23.743 27.235 0.85838 1.1685 v Velocity[Z] -27.212 19.13 -5.3434 -7.2517 v ǁVelocityǁ 0.016302 29.482 15.122 20.133 v Pressure -308.41 446.89 185.43 185.2 v k 0.0063204 9.4933 1.0257 0.69091 v omega 102.48 6.8747e+05 11438 710.05 v TurbVisc 8.4536e-08 0.010556 0.00083234 0.0010959 v CourantNb 0.0029001 1.0559 0.9396 0.99859 v FourierNb 0.0052076 10 2.825 0.32509 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1402e-05 0.01 0.00062473 0.0004908 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99938 11.017 3.7646 1.3237 INSTANT 0.224000000E-02 TIME STEP NUMBER 224 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500190E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14172E-01 0.35990E+02 Friction velocity uk : 0.43545E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10702E+03 6 0.46808E-03 0.64418E+00 0.19276E+01 c Velocity[X] 0.25729E+00 c Velocity[Y] 0.13182E+00 c Velocity[Z] 0.25507E+00 c Pressure 0.81055E-03 13 0.50588E-04 0.11449E-01 0.42773E+00 c k 0.31715E+01 6 0.20696E-05 0.46397E-01 0.93930E+01 c omega 0.26993E+05 3 0.10256E-05 0.17958E+05 0.10400E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.042 26.221 -4.4419 -6.0615 v Velocity[Y] -23.76 27.228 0.85841 1.1685 v Velocity[Z] -27.206 19.199 -5.3435 -7.2517 v ǁVelocityǁ 0.015711 29.47 15.123 20.133 v Pressure -308.75 446.99 185.44 185.21 v k 0.0063394 9.4818 1.0258 0.69163 v omega 102.22 6.8747e+05 11439 709.56 v TurbVisc 8.4522e-08 0.010556 0.00083408 0.0010996 v CourantNb 0.0027498 1.0401 0.9396 0.99859 v FourierNb 0.0052184 10 2.8242 0.32507 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1398e-05 0.01 0.00062469 0.00049079 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0008 11.02 3.7638 1.3237 INSTANT 0.225000000E-02 TIME STEP NUMBER 225 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500071E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20173E-01 0.35859E+02 Friction velocity uk : 0.43610E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10703E+03 6 0.46831E-03 0.64027E+00 0.19227E+01 c Velocity[X] 0.25613E+00 c Velocity[Y] 0.12988E+00 c Velocity[Z] 0.25426E+00 c Pressure 0.83712E-03 13 0.53198E-04 0.11824E-01 0.10389E+01 c k 0.31756E+01 6 0.20481E-05 0.45839E-01 0.93395E+01 c omega 0.26997E+05 3 0.10148E-05 0.17765E+05 0.10335E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.043 26.209 -4.4419 -6.0615 v Velocity[Y] -23.782 27.221 0.85843 1.1685 v Velocity[Z] -27.2 19.267 -5.3436 -7.2517 v ǁVelocityǁ 0.015324 29.487 15.124 20.134 v Pressure -308.93 447.35 185.5 185.27 v k 0.0063579 9.4673 1.0258 0.69234 v omega 101.96 6.8747e+05 11439 709.08 v TurbVisc 8.4495e-08 0.010556 0.00083583 0.0011034 v CourantNb 0.0028893 1.0394 0.9396 0.99859 v FourierNb 0.0052291 10 2.8234 0.32505 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1394e-05 0.01 0.00062465 0.00049078 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0015 11.016 3.763 1.3236 INSTANT 0.226000000E-02 TIME STEP NUMBER 226 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499905E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10499E+00 0.35979E+02 Friction velocity uk : 0.43673E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10704E+03 6 0.45845E-03 0.63469E+00 0.19175E+01 c Velocity[X] 0.25405E+00 c Velocity[Y] 0.12847E+00 c Velocity[Z] 0.25217E+00 c Pressure 0.83874E-03 20 0.50861E-04 0.11847E-01 0.13601E+02 c k 0.31797E+01 5 0.42904E-05 0.45281E-01 0.92857E+01 c omega 0.27001E+05 3 0.10018E-05 0.17569E+05 0.10265E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.034 26.197 -4.4418 -6.0615 v Velocity[Y] -23.8 27.214 0.85846 1.1685 v Velocity[Z] -27.19 19.332 -5.3437 -7.2517 v ǁVelocityǁ 0.015423 29.5 15.125 20.134 v Pressure -308.96 449.25 186.52 186.29 v k 0.0063701 9.4536 1.0259 0.69306 v omega 101.7 6.8747e+05 11440 708.6 v TurbVisc 8.4487e-08 0.010556 0.00083757 0.0011071 v CourantNb 0.0027466 1.0421 0.9396 0.99859 v FourierNb 0.0052398 10 2.8226 0.32504 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.139e-05 0.01 0.00062461 0.00049077 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99886 11.023 3.7622 1.3236 INSTANT 0.227000000E-02 TIME STEP NUMBER 227 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499831E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60651E-01 0.35957E+02 Friction velocity uk : 0.43715E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10704E+03 6 0.46254E-03 0.62932E+00 0.19080E+01 c Velocity[X] 0.25205E+00 c Velocity[Y] 0.12704E+00 c Velocity[Z] 0.25023E+00 c Pressure 0.81914E-03 13 0.51077E-04 0.11570E-01 0.50522E+00 c k 0.31838E+01 5 0.42083E-05 0.44743E-01 0.92333E+01 c omega 0.27005E+05 3 0.99182E-06 0.17112E+05 0.10143E+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 k a omega a Local Time Step 0.010902 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.039 26.215 -4.4418 -6.0615 v Velocity[Y] -23.818 27.206 0.85849 1.1685 v Velocity[Z] -27.173 19.399 -5.3438 -7.2517 v ǁVelocityǁ 0.014498 29.519 15.126 20.134 v Pressure -309.2 449.39 186.52 186.28 v k 0.0063794 9.4418 1.026 0.69379 v omega 101.41 6.8747e+05 11440 708.13 v TurbVisc 8.4483e-08 0.010556 0.00083932 0.0011108 v CourantNb 0.0029924 1.0468 0.9396 0.99859 v FourierNb 0.0052503 10 2.8218 0.32503 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1386e-05 0.01 0.00062457 0.00049076 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99906 11.035 3.7614 1.3236 INSTANT 0.228000000E-02 TIME STEP NUMBER 228 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499806E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10069E+00 0.36078E+02 Friction velocity uk : 0.43747E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10705E+03 6 0.46309E-03 0.62468E+00 0.19049E+01 c Velocity[X] 0.25085E+00 c Velocity[Y] 0.12548E+00 c Velocity[Z] 0.24835E+00 c Pressure 0.81557E-03 19 0.49378E-04 0.11519E-01 0.74423E+01 c k 0.31879E+01 5 0.41943E-05 0.44216E-01 0.91817E+01 c omega 0.27009E+05 3 0.98475E-06 0.16783E+05 0.10049E+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 k a omega a Local Time Step 0.010754 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.032 26.203 -4.4417 -6.0615 v Velocity[Y] -23.821 27.199 0.85851 1.1685 v Velocity[Z] -27.163 19.466 -5.3438 -7.2517 v ǁVelocityǁ 0.015767 29.523 15.127 20.134 v Pressure -309.55 448.16 186.03 185.8 v k 0.0063926 9.4318 1.0261 0.69451 v omega 101.14 6.8747e+05 11441 707.67 v TurbVisc 8.4465e-08 0.010556 0.00084106 0.0011145 v CourantNb 0.0027004 1.058 0.9396 0.99859 v FourierNb 0.0052609 10 2.821 0.32502 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1383e-05 0.01 0.00062453 0.00049075 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0008 11.014 3.7606 1.3236 INSTANT 0.229000000E-02 TIME STEP NUMBER 229 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500148E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10956E+00 0.36057E+02 Friction velocity uk : 0.43792E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10706E+03 6 0.46398E-03 0.62021E+00 0.18986E+01 c Velocity[X] 0.24899E+00 c Velocity[Y] 0.12410E+00 c Velocity[Z] 0.24712E+00 c Pressure 0.82278E-03 13 0.51905E-04 0.11621E-01 0.46118E+00 c k 0.31920E+01 5 0.41089E-05 0.43684E-01 0.91291E+01 c omega 0.27014E+05 3 0.97272E-06 0.16624E+05 0.99912E+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 k a omega a Local Time Step 0.010602 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.032 26.176 -4.4416 -6.0615 v Velocity[Y] -23.84 27.193 0.85854 1.1685 v Velocity[Z] -27.148 19.531 -5.3439 -7.2517 v ǁVelocityǁ 0.014572 29.513 15.128 20.134 v Pressure -310.04 448.21 186.02 185.79 v k 0.0064063 9.4246 1.0262 0.69524 v omega 100.88 6.8747e+05 11442 707.21 v TurbVisc 8.4447e-08 0.010556 0.00084281 0.0011182 v CourantNb 0.0028937 1.0482 0.9396 0.99859 v FourierNb 0.0052713 10 2.8203 0.32502 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1379e-05 0.01 0.00062449 0.00049074 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.001 11.041 3.7599 1.3236 INSTANT 0.230000000E-02 TIME STEP NUMBER 230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500378E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99560E-01 0.35955E+02 Friction velocity uk : 0.43839E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10707E+03 6 0.46041E-03 0.61541E+00 0.18934E+01 c Velocity[X] 0.24751E+00 c Velocity[Y] 0.12269E+00 c Velocity[Z] 0.24521E+00 c Pressure 0.82804E-03 13 0.49550E-04 0.11696E-01 0.46204E+00 c k 0.31961E+01 5 0.40989E-05 0.43166E-01 0.90774E+01 c omega 0.27018E+05 3 0.97190E-06 0.16447E+05 0.99279E+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 k a omega a Local Time Step 0.010599 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.032 26.142 -4.4415 -6.0615 v Velocity[Y] -23.863 27.185 0.85857 1.1685 v Velocity[Z] -27.143 19.596 -5.344 -7.2517 v ǁVelocityǁ 0.014927 29.531 15.129 20.134 v Pressure -310.11 448.25 186.01 185.78 v k 0.0064171 9.4186 1.0263 0.69597 v omega 100.64 6.8747e+05 11442 706.76 v TurbVisc 8.444e-08 0.010556 0.00084455 0.0011219 v CourantNb 0.0027473 1.0459 0.9396 0.99859 v FourierNb 0.0052818 10 2.8196 0.32502 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1375e-05 0.01 0.00062446 0.00049073 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0004 11.019 3.7592 1.3236 INSTANT 0.231000000E-02 TIME STEP NUMBER 231 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500504E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+00 0.35980E+02 Friction velocity uk : 0.43876E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10707E+03 6 0.46449E-03 0.61011E+00 0.18860E+01 c Velocity[X] 0.24568E+00 c Velocity[Y] 0.12073E+00 c Velocity[Z] 0.24369E+00 c Pressure 0.81655E-03 23 0.52233E-04 0.11533E-01 0.67464E+01 c k 0.32002E+01 5 0.40097E-05 0.42657E-01 0.90265E+01 c omega 0.27022E+05 3 0.96483E-06 0.16402E+05 0.99078E+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 k a omega a Local Time Step 0.010552 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.034 26.104 -4.4415 -6.0615 v Velocity[Y] -23.882 27.178 0.8586 1.1685 v Velocity[Z] -27.139 19.658 -5.344 -7.2517 v ǁVelocityǁ 0.013956 29.547 15.129 20.134 v Pressure -310.74 448.16 185.47 185.24 v k 0.0064264 9.4139 1.0264 0.6967 v omega 100.39 6.8747e+05 11443 706.31 v TurbVisc 8.4426e-08 0.010556 0.0008463 0.0011256 v CourantNb 0.0027642 1.0558 0.9396 0.99859 v FourierNb 0.0052922 10 2.8189 0.32502 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1371e-05 0.01 0.00062442 0.00049072 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0002 11.02 3.7585 1.3236 INSTANT 0.232000000E-02 TIME STEP NUMBER 232 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500135E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96639E-01 0.35972E+02 Friction velocity uk : 0.43908E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10708E+03 6 0.47322E-03 0.60581E+00 0.18818E+01 c Velocity[X] 0.24432E+00 c Velocity[Y] 0.11947E+00 c Velocity[Z] 0.24202E+00 c Pressure 0.82896E-03 18 0.50180E-04 0.11708E-01 0.20813E+01 c k 0.32042E+01 5 0.39723E-05 0.42147E-01 0.89752E+01 c omega 0.27027E+05 3 0.96072E-06 0.16353E+05 0.98738E+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 k a omega a Local Time Step 0.010582 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.006 26.061 -4.4414 -6.0615 v Velocity[Y] -23.901 27.171 0.85863 1.1685 v Velocity[Z] -27.127 19.722 -5.3441 -7.2517 v ǁVelocityǁ 0.014586 29.559 15.13 20.134 v Pressure -311.02 447.81 185.43 185.19 v k 0.0064251 9.4074 1.0265 0.69744 v omega 100.16 6.8747e+05 11443 705.87 v TurbVisc 8.4412e-08 0.010556 0.00084804 0.0011293 v CourantNb 0.0026861 1.0415 0.9396 0.99858 v FourierNb 0.0053026 10 2.8182 0.32503 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1367e-05 0.01 0.00062438 0.00049071 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0002 11.02 3.7578 1.3236 INSTANT 0.233000000E-02 TIME STEP NUMBER 233 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499953E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10116E+00 0.36080E+02 Friction velocity uk : 0.43904E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10709E+03 6 0.45960E-03 0.60223E+00 0.18785E+01 c Velocity[X] 0.24287E+00 c Velocity[Y] 0.11840E+00 c Velocity[Z] 0.24096E+00 c Pressure 0.84095E-03 10 0.50989E-04 0.11878E-01 0.40474E+00 c k 0.32083E+01 5 0.38846E-05 0.41650E-01 0.89246E+01 c omega 0.27031E+05 3 0.94302E-06 0.16098E+05 0.97916E+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 k a omega a Local Time Step 0.010488 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.011 26.018 -4.4413 -6.0615 v Velocity[Y] -23.916 27.163 0.85866 1.1685 v Velocity[Z] -27.122 19.786 -5.3442 -7.2517 v ǁVelocityǁ 0.014206 29.549 15.131 20.134 v Pressure -311.27 447.96 185.43 185.19 v k 0.006412 9.4012 1.0266 0.69818 v omega 99.935 6.8747e+05 11444 705.44 v TurbVisc 8.4404e-08 0.010556 0.00084979 0.0011329 v CourantNb 0.0028797 1.0514 0.9396 0.99858 v FourierNb 0.0053129 10 2.8175 0.32504 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1363e-05 0.01 0.00062435 0.00049071 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0003 11.026 3.7572 1.3236 INSTANT 0.234000000E-02 TIME STEP NUMBER 234 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499790E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97349E-01 0.36115E+02 Friction velocity uk : 0.43859E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10709E+03 6 0.44991E-03 0.59542E+00 0.18683E+01 c Velocity[X] 0.24061E+00 c Velocity[Y] 0.11633E+00 c Velocity[Z] 0.23847E+00 c Pressure 0.81050E-03 13 0.48691E-04 0.11448E-01 0.40731E+00 c k 0.32124E+01 5 0.38517E-05 0.41158E-01 0.88738E+01 c omega 0.27035E+05 3 0.93378E-06 0.15899E+05 0.97296E+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 k a omega a Local Time Step 0.01052 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.016 25.968 -4.4412 -6.0615 v Velocity[Y] -23.919 27.156 0.85869 1.1685 v Velocity[Z] -27.118 19.849 -5.3442 -7.2517 v ǁVelocityǁ 0.014159 29.591 15.132 20.134 v Pressure -311.33 447.99 185.44 185.2 v k 0.0064005 9.3921 1.0268 0.69891 v omega 99.728 6.8747e+05 11445 705.01 v TurbVisc 8.4401e-08 0.010556 0.00085154 0.0011366 v CourantNb 0.0026219 1.0586 0.9396 0.99858 v FourierNb 0.0053233 10 2.8169 0.32505 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1359e-05 0.01 0.00062431 0.0004907 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0012 11.012 3.7565 1.3236 INSTANT 0.235000000E-02 TIME STEP NUMBER 235 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499665E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98258E-01 0.36090E+02 Friction velocity uk : 0.43819E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10710E+03 6 0.46393E-03 0.59047E+00 0.18618E+01 c Velocity[X] 0.23885E+00 c Velocity[Y] 0.11481E+00 c Velocity[Z] 0.23682E+00 c Pressure 0.80967E-03 13 0.50236E-04 0.11436E-01 0.45293E+00 c k 0.32164E+01 5 0.37650E-05 0.40683E-01 0.88251E+01 c omega 0.27040E+05 3 0.92274E-06 0.15734E+05 0.96689E+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 k a omega a Local Time Step 0.010404 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.024 25.916 -4.4411 -6.0615 v Velocity[Y] -23.941 27.15 0.85872 1.1685 v Velocity[Z] -27.107 19.91 -5.3443 -7.2517 v ǁVelocityǁ 0.013865 29.605 15.133 20.134 v Pressure -311.57 447.84 185.46 185.22 v k 0.0063909 9.3811 1.0269 0.69966 v omega 99.532 6.8747e+05 11445 704.59 v TurbVisc 8.4402e-08 0.010556 0.00085328 0.0011403 v CourantNb 0.002816 1.0683 0.93961 0.99858 v FourierNb 0.0053335 10 2.8163 0.32507 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1356e-05 0.01 0.00062427 0.00049069 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0013 11.019 3.7559 1.3237 INSTANT 0.236000000E-02 TIME STEP NUMBER 236 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499596E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96129E-01 0.36092E+02 Friction velocity uk : 0.43787E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10711E+03 6 0.46790E-03 0.58685E+00 0.18585E+01 c Velocity[X] 0.23736E+00 c Velocity[Y] 0.11379E+00 c Velocity[Z] 0.23570E+00 c Pressure 0.83097E-03 13 0.48732E-04 0.11737E-01 0.42415E+00 c k 0.32205E+01 5 0.37373E-05 0.40215E-01 0.87763E+01 c omega 0.27044E+05 3 0.92359E-06 0.15509E+05 0.95951E+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 k a omega a Local Time Step 0.01035 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.022 25.859 -4.4411 -6.0615 v Velocity[Y] -23.962 27.132 0.85875 1.1685 v Velocity[Z] -27.099 19.969 -5.3443 -7.2517 v ǁVelocityǁ 0.014788 29.615 15.134 20.135 v Pressure -311.8 447.91 185.47 185.23 v k 0.0063832 9.3688 1.027 0.7004 v omega 99.347 6.8747e+05 11446 704.17 v TurbVisc 8.4408e-08 0.010556 0.00085503 0.001144 v CourantNb 0.0026992 1.0702 0.93961 0.99858 v FourierNb 0.0053438 10 2.8157 0.32509 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1352e-05 0.01 0.00062424 0.00049068 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0015 11.018 3.7553 1.3237 INSTANT 0.237000000E-02 TIME STEP NUMBER 237 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499571E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10256E+00 0.36192E+02 Friction velocity uk : 0.43760E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10711E+03 6 0.46350E-03 0.58287E+00 0.18546E+01 c Velocity[X] 0.23615E+00 c Velocity[Y] 0.11255E+00 c Velocity[Z] 0.23417E+00 c Pressure 0.83244E-03 13 0.48850E-04 0.11758E-01 0.43983E+00 c k 0.32245E+01 5 0.36890E-05 0.39751E-01 0.87275E+01 c omega 0.27049E+05 3 0.92456E-06 0.15406E+05 0.95548E+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 k a omega a Local Time Step 0.01022 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.005 25.801 -4.441 -6.0615 v Velocity[Y] -23.984 27.121 0.85879 1.1685 v Velocity[Z] -27.094 20.028 -5.3444 -7.2517 v ǁVelocityǁ 0.013408 29.617 15.134 20.135 v Pressure -312.2 448.05 185.49 185.24 v k 0.0063769 9.3577 1.0272 0.70115 v omega 99.149 6.8747e+05 11446 703.76 v TurbVisc 8.442e-08 0.010556 0.00085678 0.0011477 v CourantNb 0.0027792 1.0459 0.93961 0.99858 v FourierNb 0.005354 10 2.8151 0.32511 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1348e-05 0.01 0.00062421 0.00049068 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0005 11.022 3.7547 1.3237 INSTANT 0.238000000E-02 TIME STEP NUMBER 238 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499585E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91451E-01 0.36201E+02 Friction velocity uk : 0.43739E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10712E+03 6 0.46305E-03 0.57712E+00 0.18459E+01 c Velocity[X] 0.23389E+00 c Velocity[Y] 0.11077E+00 c Velocity[Z] 0.23246E+00 c Pressure 0.82084E-03 12 0.48627E-04 0.11594E-01 0.39115E+00 c k 0.32285E+01 5 0.36038E-05 0.39290E-01 0.86783E+01 c omega 0.27054E+05 3 0.91213E-06 0.15279E+05 0.95101E+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 k a omega a Local Time Step 0.010087 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.016 25.738 -4.4409 -6.0615 v Velocity[Y] -24.005 27.112 0.85882 1.1685 v Velocity[Z] -27.089 20.081 -5.3445 -7.2517 v ǁVelocityǁ 0.01353 29.609 15.135 20.135 v Pressure -312.51 448.06 185.5 185.26 v k 0.0063717 9.349 1.0274 0.70189 v omega 98.936 6.8747e+05 11447 703.36 v TurbVisc 8.4429e-08 0.010556 0.00085852 0.0011514 v CourantNb 0.0026733 1.0424 0.93961 0.99858 v FourierNb 0.0053642 10 2.8145 0.32514 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1344e-05 0.01 0.00062417 0.00049067 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0009 11.035 3.7541 1.3237 INSTANT 0.239000000E-02 TIME STEP NUMBER 239 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499639E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94023E-01 0.36247E+02 Friction velocity uk : 0.43721E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10713E+03 6 0.46484E-03 0.57298E+00 0.18405E+01 c Velocity[X] 0.23252E+00 c Velocity[Y] 0.10956E+00 c Velocity[Z] 0.23090E+00 c Pressure 0.82986E-03 13 0.50515E-04 0.11721E-01 0.11777E+01 c k 0.32326E+01 5 0.35638E-05 0.38845E-01 0.86308E+01 c omega 0.27059E+05 3 0.89976E-06 0.14920E+05 0.94030E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.012 25.673 -4.4408 -6.0615 v Velocity[Y] -24.012 27.104 0.85885 1.1685 v Velocity[Z] -27.079 20.136 -5.3445 -7.2517 v ǁVelocityǁ 0.012893 29.647 15.136 20.135 v Pressure -312.67 448.35 185.59 185.34 v k 0.0063686 9.3386 1.0275 0.70264 v omega 98.736 6.8747e+05 11448 702.96 v TurbVisc 8.4435e-08 0.010556 0.00086027 0.0011551 v CourantNb 0.0026519 1.0843 0.93961 0.99858 v FourierNb 0.0053743 10 2.8139 0.32516 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.134e-05 0.0099841 0.00062414 0.00049066 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0003 11.035 3.7536 1.3237 INSTANT 0.240000000E-02 TIME STEP NUMBER 240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499737E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88961E-01 0.36237E+02 Friction velocity uk : 0.43710E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10713E+03 6 0.46362E-03 0.56877E+00 0.18364E+01 c Velocity[X] 0.23095E+00 c Velocity[Y] 0.10819E+00 c Velocity[Z] 0.22963E+00 c Pressure 0.83033E-03 10 0.46250E-04 0.11728E-01 0.43707E+00 c k 0.32366E+01 5 0.35248E-05 0.38404E-01 0.85834E+01 c omega 0.27063E+05 3 0.90387E-06 0.14911E+05 0.93827E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.019 25.604 -4.4407 -6.0615 v Velocity[Y] -24.029 27.096 0.85889 1.1685 v Velocity[Z] -27.076 20.188 -5.3446 -7.2517 v ǁVelocityǁ 0.014066 29.64 15.137 20.135 v Pressure -312.68 448.41 185.6 185.36 v k 0.0063676 9.3308 1.0277 0.70339 v omega 98.546 6.8747e+05 11448 702.56 v TurbVisc 8.4454e-08 0.010556 0.00086201 0.0011588 v CourantNb 0.0025309 1.0658 0.93962 0.99858 v FourierNb 0.0053844 10 2.8134 0.32519 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1336e-05 0.0098759 0.0006241 0.00049066 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0013 11.03 3.753 1.3238 INSTANT 0.241000000E-02 TIME STEP NUMBER 241 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499844E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97258E-01 0.36148E+02 Friction velocity uk : 0.43707E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10714E+03 6 0.46282E-03 0.56402E+00 0.18298E+01 c Velocity[X] 0.22920E+00 c Velocity[Y] 0.10695E+00 c Velocity[Z] 0.22787E+00 c Pressure 0.83050E-03 11 0.48136E-04 0.11730E-01 0.38556E+00 c k 0.32406E+01 5 0.34469E-05 0.37966E-01 0.85357E+01 c omega 0.27068E+05 3 0.88757E-06 0.14715E+05 0.93214E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.021 25.565 -4.4406 -6.0615 v Velocity[Y] -24.045 27.089 0.85892 1.1685 v Velocity[Z] -27.072 20.24 -5.3446 -7.2517 v ǁVelocityǁ 0.013018 29.652 15.138 20.135 v Pressure -312.85 448.33 185.61 185.37 v k 0.0063686 9.3205 1.0279 0.70415 v omega 98.366 6.8747e+05 11449 702.17 v TurbVisc 8.4479e-08 0.010556 0.00086376 0.0011625 v CourantNb 0.0026912 1.0489 0.93962 0.99858 v FourierNb 0.0053945 10 2.8129 0.32523 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1332e-05 0.0097967 0.00062407 0.00049065 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0001 11.022 3.7525 1.3238 INSTANT 0.242000000E-02 TIME STEP NUMBER 242 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499939E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89664E-01 0.36221E+02 Friction velocity uk : 0.43710E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10715E+03 6 0.46324E-03 0.55977E+00 0.18240E+01 c Velocity[X] 0.22798E+00 c Velocity[Y] 0.10562E+00 c Velocity[Z] 0.22617E+00 c Pressure 0.82768E-03 10 0.46006E-04 0.11690E-01 0.37969E+00 c k 0.32446E+01 5 0.34001E-05 0.37535E-01 0.84884E+01 c omega 0.27073E+05 3 0.88190E-06 0.14573E+05 0.92682E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.022 25.529 -4.4405 -6.0615 v Velocity[Y] -24.065 27.081 0.85896 1.1685 v Velocity[Z] -27.061 20.288 -5.3447 -7.2517 v ǁVelocityǁ 0.012495 29.656 15.138 20.135 v Pressure -312.88 448.33 185.61 185.37 v k 0.0063701 9.3096 1.028 0.7049 v omega 98.18 6.8747e+05 11450 701.79 v TurbVisc 8.4507e-08 0.010556 0.00086551 0.0011661 v CourantNb 0.0026275 1.0816 0.93962 0.99858 v FourierNb 0.0054046 10 2.8123 0.32526 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1329e-05 0.009746 0.00062403 0.00049064 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0022 11.026 3.752 1.3238 INSTANT 0.243000000E-02 TIME STEP NUMBER 243 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500008E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86190E-01 0.36213E+02 Friction velocity uk : 0.43715E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10715E+03 6 0.46936E-03 0.55573E+00 0.18188E+01 c Velocity[X] 0.22652E+00 c Velocity[Y] 0.10434E+00 c Velocity[Z] 0.22487E+00 c Pressure 0.82085E-03 10 0.48825E-04 0.11594E-01 0.38949E+00 c k 0.32486E+01 5 0.33682E-05 0.37120E-01 0.84429E+01 c omega 0.27078E+05 3 0.88847E-06 0.14478E+05 0.92301E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.017 25.493 -4.4404 -6.0615 v Velocity[Y] -24.084 27.077 0.85899 1.1685 v Velocity[Z] -27.06 20.352 -5.3447 -7.2517 v ǁVelocityǁ 0.01302 29.661 15.139 20.135 v Pressure -313.2 448.4 185.62 185.37 v k 0.0063734 9.2992 1.0282 0.70566 v omega 97.986 6.8747e+05 11450 701.41 v TurbVisc 8.4517e-08 0.010556 0.00086725 0.0011698 v CourantNb 0.0026921 1.04 0.93962 0.99858 v FourierNb 0.0054146 10 2.8118 0.3253 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1325e-05 0.0096517 0.000624 0.00049064 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99964 11.017 3.7515 1.3239 INSTANT 0.244000000E-02 TIME STEP NUMBER 244 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500076E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90330E-01 0.36283E+02 Friction velocity uk : 0.43727E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10716E+03 6 0.46632E-03 0.55162E+00 0.18136E+01 c Velocity[X] 0.22494E+00 c Velocity[Y] 0.10316E+00 c Velocity[Z] 0.22352E+00 c Pressure 0.82455E-03 10 0.44762E-04 0.11646E-01 0.40804E+00 c k 0.32526E+01 5 0.33249E-05 0.36703E-01 0.83964E+01 c omega 0.27083E+05 3 0.87853E-06 0.14408E+05 0.91936E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.003 25.471 -4.4404 -6.0615 v Velocity[Y] -24.089 27.073 0.85903 1.1685 v Velocity[Z] -27.054 20.422 -5.3448 -7.2517 v ǁVelocityǁ 0.012813 29.692 15.14 20.135 v Pressure -313.45 448.45 185.62 185.38 v k 0.0063773 9.288 1.0284 0.70642 v omega 97.8 6.8747e+05 11451 701.04 v TurbVisc 8.4542e-08 0.010556 0.000869 0.0011735 v CourantNb 0.0025385 1.0381 0.93962 0.99858 v FourierNb 0.0054247 10 2.8113 0.32534 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1321e-05 0.0095735 0.00062397 0.00049063 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0024 11.028 3.751 1.3239 INSTANT 0.245000000E-02 TIME STEP NUMBER 245 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500116E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88646E-01 0.36326E+02 Friction velocity uk : 0.43740E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10717E+03 6 0.46802E-03 0.54709E+00 0.18068E+01 c Velocity[X] 0.22333E+00 c Velocity[Y] 0.10203E+00 c Velocity[Z] 0.22174E+00 c Pressure 0.81996E-03 10 0.47685E-04 0.11581E-01 0.38710E+00 c k 0.32566E+01 5 0.32566E-05 0.36289E-01 0.83497E+01 c omega 0.27088E+05 3 0.86550E-06 0.14083E+05 0.90947E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.013 25.455 -4.4403 -6.0615 v Velocity[Y] -24.105 27.068 0.85906 1.1685 v Velocity[Z] -27.052 20.492 -5.3448 -7.2517 v ǁVelocityǁ 0.012057 29.681 15.141 20.135 v Pressure -313.64 448.56 185.62 185.37 v k 0.0063827 9.2782 1.0286 0.70718 v omega 97.622 6.8747e+05 11452 700.67 v TurbVisc 8.4557e-08 0.010556 0.00087075 0.0011772 v CourantNb 0.002742 1.0466 0.93963 0.99858 v FourierNb 0.0054346 10 2.8109 0.32539 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1317e-05 0.00951 0.00062394 0.00049063 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99985 11.015 3.7505 1.324 INSTANT 0.246000000E-02 TIME STEP NUMBER 246 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500146E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80704E-01 0.36195E+02 Friction velocity uk : 0.43758E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10717E+03 6 0.47083E-03 0.54345E+00 0.18032E+01 c Velocity[X] 0.22199E+00 c Velocity[Y] 0.10062E+00 c Velocity[Z] 0.22084E+00 c Pressure 0.83120E-03 11 0.45667E-04 0.11740E-01 0.38550E+00 c k 0.32606E+01 5 0.32410E-05 0.35894E-01 0.83053E+01 c omega 0.27093E+05 3 0.87726E-06 0.13922E+05 0.90411E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.013 25.405 -4.4402 -6.0615 v Velocity[Y] -24.125 27.065 0.8591 1.1685 v Velocity[Z] -27.047 20.56 -5.3449 -7.2517 v ǁVelocityǁ 0.011479 29.689 15.142 20.135 v Pressure -313.63 448.54 185.62 185.37 v k 0.0063886 9.2666 1.0288 0.70795 v omega 97.435 6.8747e+05 11452 700.3 v TurbVisc 8.4583e-08 0.010556 0.00087249 0.0011809 v CourantNb 0.0025515 1.0347 0.93963 0.99858 v FourierNb 0.0054446 10 2.8104 0.32543 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1313e-05 0.0094831 0.0006239 0.00049062 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0024 11.018 3.75 1.324 INSTANT 0.247000000E-02 TIME STEP NUMBER 247 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500134E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68198E-01 0.36232E+02 Friction velocity uk : 0.43779E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10718E+03 6 0.46425E-03 0.53908E+00 0.17965E+01 c Velocity[X] 0.22049E+00 c Velocity[Y] 0.99521E-01 c Velocity[Z] 0.21907E+00 c Pressure 0.83055E-03 10 0.45443E-04 0.11731E-01 0.36055E+00 c k 0.32645E+01 5 0.31909E-05 0.35497E-01 0.82599E+01 c omega 0.27098E+05 3 0.85799E-06 0.13817E+05 0.89990E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.021 25.374 -4.4401 -6.0615 v Velocity[Y] -24.139 27.061 0.85914 1.1685 v Velocity[Z] -27.046 20.626 -5.3449 -7.2517 v ǁVelocityǁ 0.012484 29.688 15.142 20.136 v Pressure -313.84 448.63 185.61 185.37 v k 0.0063955 9.2565 1.029 0.70871 v omega 97.242 6.8747e+05 11453 699.94 v TurbVisc 8.4601e-08 0.010556 0.00087424 0.0011845 v CourantNb 0.0025957 1.0407 0.93963 0.99858 v FourierNb 0.0054546 10 2.8099 0.32548 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1309e-05 0.0093254 0.00062387 0.00049062 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0002 11.017 3.7496 1.3241 INSTANT 0.248000000E-02 TIME STEP NUMBER 248 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500120E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22897E-01 0.36296E+02 Friction velocity uk : 0.43802E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10718E+03 6 0.46335E-03 0.53477E+00 0.17900E+01 c Velocity[X] 0.21886E+00 c Velocity[Y] 0.98502E-01 c Velocity[Z] 0.21742E+00 c Pressure 0.82504E-03 10 0.44721E-04 0.11653E-01 0.37256E+00 c k 0.32685E+01 5 0.31607E-05 0.35107E-01 0.82148E+01 c omega 0.27103E+05 3 0.85654E-06 0.13609E+05 0.89292E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.018 25.343 -4.44 -6.0615 v Velocity[Y] -24.147 27.057 0.85917 1.1685 v Velocity[Z] -27.04 20.69 -5.345 -7.2517 v ǁVelocityǁ 0.011488 29.693 15.143 20.136 v Pressure -313.7 448.59 185.61 185.37 v k 0.0064021 9.2483 1.0292 0.70948 v omega 97.032 6.8747e+05 11454 699.58 v TurbVisc 8.4621e-08 0.010556 0.00087598 0.0011882 v CourantNb 0.0025535 1.07 0.93963 0.99858 v FourierNb 0.0054646 10 2.8095 0.32553 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1305e-05 0.009286 0.00062384 0.00049061 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0029 11.011 3.7491 1.3241 INSTANT 0.249000000E-02 TIME STEP NUMBER 249 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500083E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30888E-01 0.36245E+02 Friction velocity uk : 0.43825E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10719E+03 6 0.46833E-03 0.53079E+00 0.17862E+01 c Velocity[X] 0.21718E+00 c Velocity[Y] 0.97221E-01 c Velocity[Z] 0.21638E+00 c Pressure 0.82053E-03 12 0.45350E-04 0.11589E-01 0.41766E+00 c k 0.32725E+01 5 0.31591E-05 0.34728E-01 0.81709E+01 c omega 0.27108E+05 3 0.86468E-06 0.13513E+05 0.88883E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.019 25.285 -4.4399 -6.0615 v Velocity[Y] -24.165 27.054 0.85921 1.1685 v Velocity[Z] -27.039 20.749 -5.345 -7.2517 v ǁVelocityǁ 0.010861 29.698 15.144 20.136 v Pressure -314.05 448.61 185.61 185.36 v k 0.0064098 9.2381 1.0295 0.71025 v omega 96.818 6.8747e+05 11454 699.23 v TurbVisc 8.4629e-08 0.010556 0.00087773 0.0011919 v CourantNb 0.0026613 1.0412 0.93964 0.99858 v FourierNb 0.0054746 10 2.8091 0.32558 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1301e-05 0.0092356 0.0006238 0.0004906 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0006 11.019 3.7487 1.3242 INSTANT 0.250000000E-02 TIME STEP NUMBER 250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500050E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68436E-01 0.36393E+02 Friction velocity uk : 0.43851E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10720E+03 6 0.46685E-03 0.52690E+00 0.17792E+01 c Velocity[X] 0.21620E+00 c Velocity[Y] 0.95944E-01 c Velocity[Z] 0.21475E+00 c Pressure 0.81508E-03 11 0.45309E-04 0.11512E-01 0.41446E+00 c k 0.32765E+01 5 0.31236E-05 0.34349E-01 0.81265E+01 c omega 0.27113E+05 3 0.85881E-06 0.13466E+05 0.88589E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.996 25.237 -4.4398 -6.0615 v Velocity[Y] -24.17 27.05 0.85925 1.1685 v Velocity[Z] -27.034 20.805 -5.3451 -7.2517 v ǁVelocityǁ 0.011246 29.684 15.145 20.136 v Pressure -314.05 448.41 185.6 185.35 v k 0.0064137 9.2311 1.0297 0.71102 v omega 96.606 6.8747e+05 11455 698.89 v TurbVisc 8.4654e-08 0.010556 0.00087947 0.0011956 v CourantNb 0.002674 1.0327 0.93964 0.99858 v FourierNb 0.0054845 10 2.8086 0.32564 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1296e-05 0.009156 0.00062377 0.0004906 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0014 11.02 3.7483 1.3242 INSTANT 0.251000000E-02 TIME STEP NUMBER 251 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500003E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77137E-01 0.36364E+02 Friction velocity uk : 0.43865E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10720E+03 6 0.46707E-03 0.52328E+00 0.17737E+01 c Velocity[X] 0.21490E+00 c Velocity[Y] 0.95005E-01 c Velocity[Z] 0.21338E+00 c Pressure 0.81921E-03 13 0.45913E-04 0.11571E-01 0.55946E+00 c k 0.32804E+01 5 0.30794E-05 0.33974E-01 0.80820E+01 c omega 0.27118E+05 3 0.84115E-06 0.13216E+05 0.87719E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.009 25.185 -4.4397 -6.0615 v Velocity[Y] -24.198 27.046 0.85928 1.1685 v Velocity[Z] -27.032 20.856 -5.3451 -7.2517 v ǁVelocityǁ 0.0116 29.697 15.145 20.136 v Pressure -314.19 448.46 185.58 185.33 v k 0.0064124 9.2235 1.0299 0.71179 v omega 96.405 6.8747e+05 11456 698.54 v TurbVisc 8.4683e-08 0.010556 0.00088122 0.0011992 v CourantNb 0.0026865 1.0333 0.93964 0.99858 v FourierNb 0.0054944 10 2.8082 0.32569 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1293e-05 0.0090856 0.00062374 0.0004906 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0012 11.016 3.7479 1.3243 INSTANT 0.252000000E-02 TIME STEP NUMBER 252 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499960E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80109E-01 0.36199E+02 Friction velocity uk : 0.43860E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10721E+03 6 0.47446E-03 0.52047E+00 0.17712E+01 c Velocity[X] 0.21373E+00 c Velocity[Y] 0.94141E-01 c Velocity[Z] 0.21260E+00 c Pressure 0.82639E-03 13 0.43745E-04 0.11672E-01 0.51803E+00 c k 0.32844E+01 5 0.30784E-05 0.33609E-01 0.80384E+01 c omega 0.27123E+05 3 0.84708E-06 0.13140E+05 0.87449E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.017 25.14 -4.4396 -6.0615 v Velocity[Y] -24.217 27.043 0.85932 1.1685 v Velocity[Z] -27.027 20.903 -5.3452 -7.2517 v ǁVelocityǁ 0.010549 29.708 15.146 20.136 v Pressure -314.24 448.3 185.57 185.32 v k 0.0064146 9.2172 1.0301 0.71257 v omega 96.21 6.8747e+05 11456 698.21 v TurbVisc 8.4704e-08 0.010556 0.00088296 0.0012029 v CourantNb 0.0025283 1.0396 0.93965 0.99858 v FourierNb 0.0055043 10 2.8078 0.32575 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1289e-05 0.009043 0.00062371 0.00049059 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0014 11.02 3.7475 1.3243 INSTANT 0.253000000E-02 TIME STEP NUMBER 253 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499910E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72728E-01 0.36270E+02 Friction velocity uk : 0.43868E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10721E+03 6 0.46756E-03 0.51636E+00 0.17648E+01 c Velocity[X] 0.21224E+00 c Velocity[Y] 0.93130E-01 c Velocity[Z] 0.21099E+00 c Pressure 0.82955E-03 13 0.44487E-04 0.11716E-01 0.43482E+00 c k 0.32884E+01 5 0.30447E-05 0.33247E-01 0.79948E+01 c omega 0.27129E+05 3 0.84179E-06 0.13001E+05 0.86958E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.026 25.101 -4.4395 -6.0615 v Velocity[Y] -24.235 27.04 0.85936 1.1685 v Velocity[Z] -27.026 20.946 -5.3452 -7.2517 v ǁVelocityǁ 0.0097788 29.717 15.147 20.136 v Pressure -314.47 448.31 185.57 185.32 v k 0.0064151 9.2098 1.0304 0.71334 v omega 95.974 6.8747e+05 11457 697.87 v TurbVisc 8.4711e-08 0.010556 0.00088471 0.0012066 v CourantNb 0.0026619 1.0493 0.93965 0.99858 v FourierNb 0.0055142 10 2.8074 0.32581 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1285e-05 0.0089502 0.00062368 0.00049059 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.001 11.02 3.7471 1.3244 INSTANT 0.254000000E-02 TIME STEP NUMBER 254 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499879E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65605E-01 0.36260E+02 Friction velocity uk : 0.43870E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10722E+03 6 0.46422E-03 0.51212E+00 0.17578E+01 c Velocity[X] 0.21079E+00 c Velocity[Y] 0.91720E-01 c Velocity[Z] 0.20960E+00 c Pressure 0.81947E-03 13 0.43529E-04 0.11574E-01 0.59639E+00 c k 0.32923E+01 5 0.30118E-05 0.32891E-01 0.79515E+01 c omega 0.27134E+05 3 0.83903E-06 0.12859E+05 0.86409E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.02 25.036 -4.4394 -6.0615 v Velocity[Y] -24.245 27.037 0.8594 1.1685 v Velocity[Z] -27.021 20.985 -5.3453 -7.2517 v ǁVelocityǁ 0.0106 29.707 15.148 20.136 v Pressure -314.09 448.28 185.58 185.33 v k 0.0064148 9.203 1.0306 0.71412 v omega 95.753 6.8747e+05 11458 697.54 v TurbVisc 8.4728e-08 0.010556 0.00088645 0.0012103 v CourantNb 0.0026331 1.0405 0.93965 0.99858 v FourierNb 0.0055241 10 2.8071 0.32587 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1281e-05 0.0089767 0.00062364 0.00049058 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0025 11.012 3.7467 1.3245 INSTANT 0.255000000E-02 TIME STEP NUMBER 255 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499852E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73417E-01 0.36335E+02 Friction velocity uk : 0.43869E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10723E+03 6 0.47431E-03 0.50911E+00 0.17537E+01 c Velocity[X] 0.20981E+00 c Velocity[Y] 0.90890E-01 c Velocity[Z] 0.20841E+00 c Pressure 0.82826E-03 12 0.45360E-04 0.11698E-01 0.42842E+00 c k 0.32963E+01 5 0.29722E-05 0.32539E-01 0.79085E+01 c omega 0.27139E+05 3 0.82862E-06 0.12780E+05 0.86083E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.003 24.99 -4.4393 -6.0615 v Velocity[Y] -24.245 27.034 0.85944 1.1685 v Velocity[Z] -27.019 21.021 -5.3453 -7.2517 v ǁVelocityǁ 0.010503 29.717 15.149 20.136 v Pressure -313.89 448.23 185.59 185.33 v k 0.0064186 9.1927 1.0309 0.71491 v omega 95.547 6.8747e+05 11459 697.22 v TurbVisc 8.4735e-08 0.010556 0.0008882 0.0012139 v CourantNb 0.0024433 1.0379 0.93965 0.99858 v FourierNb 0.005534 10 2.8067 0.32594 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1278e-05 0.0088745 0.00062361 0.00049058 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0015 11.016 3.7463 1.3245 INSTANT 0.256000000E-02 TIME STEP NUMBER 256 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499848E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72090E-01 0.36308E+02 Friction velocity uk : 0.43882E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10723E+03 6 0.47165E-03 0.50612E+00 0.17501E+01 c Velocity[X] 0.20889E+00 c Velocity[Y] 0.89831E-01 c Velocity[Z] 0.20740E+00 c Pressure 0.82580E-03 13 0.43089E-04 0.11664E-01 0.44100E+00 c k 0.33003E+01 5 0.29766E-05 0.32198E-01 0.78663E+01 c omega 0.27145E+05 3 0.83631E-06 0.12724E+05 0.85791E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.01 24.942 -4.4392 -6.0615 v Velocity[Y] -24.255 27.031 0.85948 1.1685 v Velocity[Z] -27.018 21.051 -5.3454 -7.2517 v ǁVelocityǁ 0.0099166 29.726 15.149 20.136 v Pressure -313.86 448.15 185.6 185.34 v k 0.0064224 9.1829 1.0311 0.71569 v omega 95.353 6.8747e+05 11459 696.9 v TurbVisc 8.4733e-08 0.010556 0.00088994 0.0012176 v CourantNb 0.0026016 1.0342 0.93966 0.99858 v FourierNb 0.0055438 10 2.8063 0.326 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1274e-05 0.0089012 0.00062358 0.00049057 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.003 11.021 3.746 1.3246 INSTANT 0.257000000E-02 TIME STEP NUMBER 257 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499822E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68592E-01 0.36291E+02 Friction velocity uk : 0.43894E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10724E+03 6 0.47389E-03 0.50149E+00 0.17424E+01 c Velocity[X] 0.20715E+00 c Velocity[Y] 0.88606E-01 c Velocity[Z] 0.20573E+00 c Pressure 0.81963E-03 13 0.43492E-04 0.11576E-01 0.40618E+00 c k 0.33042E+01 5 0.29452E-05 0.31857E-01 0.78236E+01 c omega 0.27150E+05 3 0.81752E-06 0.12527E+05 0.85037E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.015 24.916 -4.4391 -6.0615 v Velocity[Y] -24.272 27.027 0.85952 1.1685 v Velocity[Z] -27.012 21.076 -5.3454 -7.2517 v ǁVelocityǁ 0.01031 29.73 15.15 20.136 v Pressure -313.88 448.16 185.61 185.36 v k 0.0064251 9.1841 1.0314 0.71647 v omega 95.164 6.8747e+05 11460 696.58 v TurbVisc 8.4731e-08 0.010556 0.00089169 0.0012213 v CourantNb 0.0025331 1.035 0.93966 0.99858 v FourierNb 0.0055537 10 2.806 0.32607 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.127e-05 0.0088293 0.00062355 0.00049057 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0022 11.024 3.7456 1.3247 INSTANT 0.258000000E-02 TIME STEP NUMBER 258 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499797E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70184E-01 0.36294E+02 Friction velocity uk : 0.43903E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10724E+03 6 0.47405E-03 0.49885E+00 0.17385E+01 c Velocity[X] 0.20621E+00 c Velocity[Y] 0.88035E-01 c Velocity[Z] 0.20461E+00 c Pressure 0.82838E-03 12 0.42258E-04 0.11700E-01 0.42529E+00 c k 0.33082E+01 5 0.29296E-05 0.31524E-01 0.77819E+01 c omega 0.27156E+05 3 0.81733E-06 0.12448E+05 0.84704E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.011 24.894 -4.439 -6.0615 v Velocity[Y] -24.289 27.024 0.85956 1.1685 v Velocity[Z] -27.009 21.096 -5.3455 -7.2517 v ǁVelocityǁ 0.0085985 29.717 15.151 20.136 v Pressure -313.82 448.11 185.63 185.37 v k 0.0064301 9.2054 1.0317 0.71726 v omega 94.977 6.8747e+05 11461 696.27 v TurbVisc 8.474e-08 0.010556 0.00089343 0.001225 v CourantNb 0.0024858 1.0336 0.93966 0.99858 v FourierNb 0.0055636 10 2.8056 0.32614 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1266e-05 0.0087579 0.00062352 0.00049056 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0024 11.02 3.7453 1.3247 INSTANT 0.259000000E-02 TIME STEP NUMBER 259 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499748E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39244E-01 0.36288E+02 Friction velocity uk : 0.43921E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10725E+03 6 0.47512E-03 0.49583E+00 0.17329E+01 c Velocity[X] 0.20531E+00 c Velocity[Y] 0.86992E-01 c Velocity[Z] 0.20353E+00 c Pressure 0.82403E-03 25 0.42676E-04 0.11638E-01 0.10260E+02 c k 0.33121E+01 5 0.28903E-05 0.31192E-01 0.77400E+01 c omega 0.27161E+05 3 0.81076E-06 0.12267E+05 0.84059E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.014 24.837 -4.4389 -6.0615 v Velocity[Y] -24.284 27.021 0.8596 1.1685 v Velocity[Z] -27.008 21.111 -5.3455 -7.2517 v ǁVelocityǁ 0.0097514 29.773 15.152 20.137 v Pressure -313.5 449.19 186.47 186.21 v k 0.0064358 9.2268 1.0319 0.71805 v omega 94.792 6.8747e+05 11462 695.96 v TurbVisc 8.4736e-08 0.010556 0.00089518 0.0012286 v CourantNb 0.0026896 1.0445 0.93967 0.99858 v FourierNb 0.0055735 10 2.8053 0.32621 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1262e-05 0.0086714 0.00062349 0.00049056 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0023 11.01 3.745 1.3248 INSTANT 0.260000000E-02 TIME STEP NUMBER 260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499901E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42466E-01 0.36433E+02 Friction velocity uk : 0.43940E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10725E+03 6 0.47937E-03 0.49284E+00 0.17315E+01 c Velocity[X] 0.20402E+00 c Velocity[Y] 0.86235E-01 c Velocity[Z] 0.20259E+00 c Pressure 0.82331E-03 10 0.42166E-04 0.11628E-01 0.35341E+00 c k 0.33161E+01 5 0.28812E-05 0.30870E-01 0.76989E+01 c omega 0.27167E+05 3 0.81949E-06 0.12266E+05 0.83995E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.019 24.814 -4.4388 -6.0615 v Velocity[Y] -24.3 27.018 0.85964 1.1685 v Velocity[Z] -27.001 21.121 -5.3456 -7.2517 v ǁVelocityǁ 0.010537 29.756 15.152 20.137 v Pressure -313.32 449.21 186.46 186.21 v k 0.0064379 9.251 1.0322 0.71884 v omega 94.62 6.8747e+05 11462 695.65 v TurbVisc 8.4731e-08 0.010556 0.00089692 0.0012323 v CourantNb 0.0025317 1.039 0.93967 0.99858 v FourierNb 0.0055833 10 2.805 0.32629 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1258e-05 0.0086101 0.00062346 0.00049056 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0023 11.031 3.7447 1.3249 INSTANT 0.261000000E-02 TIME STEP NUMBER 261 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500091E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21806E-01 0.36271E+02 Friction velocity uk : 0.43947E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10726E+03 6 0.47473E-03 0.48977E+00 0.17235E+01 c Velocity[X] 0.20300E+00 c Velocity[Y] 0.85284E-01 c Velocity[Z] 0.20149E+00 c Pressure 0.83347E-03 10 0.43087E-04 0.11772E-01 0.42140E+00 c k 0.33200E+01 5 0.28571E-05 0.30546E-01 0.76575E+01 c omega 0.27172E+05 3 0.81137E-06 0.12162E+05 0.83510E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.006 24.78 -4.4387 -6.0615 v Velocity[Y] -24.319 27.015 0.85968 1.1685 v Velocity[Z] -26.998 21.125 -5.3456 -7.2517 v ǁVelocityǁ 0.0082788 29.758 15.153 20.137 v Pressure -313.41 449.12 186.44 186.19 v k 0.0064402 9.2699 1.0325 0.71963 v omega 94.458 6.8747e+05 11463 695.35 v TurbVisc 8.4726e-08 0.010556 0.00089867 0.001236 v CourantNb 0.0026595 1.0355 0.93967 0.99858 v FourierNb 0.0055932 10 2.8047 0.32636 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1254e-05 0.0085259 0.00062342 0.00049055 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0021 11.016 3.7444 1.3249 INSTANT 0.262000000E-02 TIME STEP NUMBER 262 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500305E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29625E-01 0.36312E+02 Friction velocity uk : 0.43955E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10727E+03 6 0.47322E-03 0.48639E+00 0.17200E+01 c Velocity[X] 0.20202E+00 c Velocity[Y] 0.84137E-01 c Velocity[Z] 0.20024E+00 c Pressure 0.82954E-03 21 0.41147E-04 0.11716E-01 0.12276E+02 c k 0.33240E+01 5 0.28325E-05 0.30228E-01 0.76164E+01 c omega 0.27178E+05 3 0.80708E-06 0.12092E+05 0.83228E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.005 24.749 -4.4386 -6.0615 v Velocity[Y] -24.338 27.012 0.85972 1.1685 v Velocity[Z] -26.996 21.124 -5.3457 -7.2517 v ǁVelocityǁ 0.0096892 29.748 15.154 20.137 v Pressure -314.09 447.71 185.44 185.18 v k 0.0064443 9.2919 1.0327 0.72043 v omega 94.305 6.8747e+05 11464 695.05 v TurbVisc 8.4732e-08 0.010556 0.00090041 0.0012397 v CourantNb 0.0025583 1.0344 0.93967 0.99858 v FourierNb 0.0056031 10 2.8044 0.32644 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.125e-05 0.0084528 0.00062339 0.00049055 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0024 11.012 3.744 1.325 INSTANT 0.263000000E-02 TIME STEP NUMBER 263 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500163E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20212E-01 0.36438E+02 Friction velocity uk : 0.43969E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10727E+03 6 0.47302E-03 0.48253E+00 0.17120E+01 c Velocity[X] 0.20052E+00 c Velocity[Y] 0.83301E-01 c Velocity[Z] 0.19871E+00 c Pressure 0.82209E-03 13 0.40553E-04 0.11611E-01 0.44896E+00 c k 0.33280E+01 5 0.27813E-05 0.29914E-01 0.75757E+01 c omega 0.27183E+05 3 0.79358E-06 0.11944E+05 0.82683E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.006 24.688 -4.4385 -6.0615 v Velocity[Y] -24.343 27.008 0.85976 1.1685 v Velocity[Z] -26.989 21.117 -5.3457 -7.2517 v ǁVelocityǁ 0.0097214 29.732 15.155 20.137 v Pressure -314.03 447.65 185.45 185.19 v k 0.0064495 9.3085 1.033 0.72123 v omega 94.127 6.8747e+05 11465 694.76 v TurbVisc 8.4725e-08 0.010556 0.00090215 0.0012433 v CourantNb 0.0025797 1.0404 0.93968 0.99858 v FourierNb 0.0056129 10 2.8041 0.32652 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1246e-05 0.008333 0.00062336 0.00049055 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0016 11.024 3.7438 1.3251 INSTANT 0.264000000E-02 TIME STEP NUMBER 264 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499978E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51689E-01 0.36354E+02 Friction velocity uk : 0.43987E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10728E+03 6 0.48694E-03 0.47992E+00 0.17087E+01 c Velocity[X] 0.19941E+00 c Velocity[Y] 0.82436E-01 c Velocity[Z] 0.19807E+00 c Pressure 0.82710E-03 19 0.40642E-04 0.11682E-01 0.29373E+01 c k 0.33319E+01 5 0.27682E-05 0.29605E-01 0.75352E+01 c omega 0.27189E+05 3 0.79023E-06 0.11878E+05 0.82351E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.012 24.663 -4.4384 -6.0615 v Velocity[Y] -24.363 27.005 0.85981 1.1685 v Velocity[Z] -26.985 21.101 -5.3458 -7.2517 v ǁVelocityǁ 0.0081134 29.739 15.155 20.137 v Pressure -313.87 447.8 185.66 185.4 v k 0.0064572 9.3275 1.0333 0.72203 v omega 93.953 6.8747e+05 11465 694.47 v TurbVisc 8.4728e-08 0.010556 0.00090389 0.001247 v CourantNb 0.0023965 1.0352 0.93968 0.99858 v FourierNb 0.0056229 10 2.8038 0.32659 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1242e-05 0.0082687 0.00062333 0.00049054 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0026 11.035 3.7435 1.3252 INSTANT 0.265000000E-02 TIME STEP NUMBER 265 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499683E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56214E-01 0.36297E+02 Friction velocity uk : 0.44013E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10728E+03 6 0.47950E-03 0.47781E+00 0.17073E+01 c Velocity[X] 0.19880E+00 c Velocity[Y] 0.81763E-01 c Velocity[Z] 0.19724E+00 c Pressure 0.82879E-03 26 0.41355E-04 0.11706E-01 0.99215E+01 c k 0.33359E+01 5 0.27592E-05 0.29300E-01 0.74951E+01 c omega 0.27195E+05 3 0.79259E-06 0.11709E+05 0.81768E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.018 24.63 -4.4383 -6.0615 v Velocity[Y] -24.376 27.002 0.85985 1.1685 v Velocity[Z] -26.983 21.08 -5.3458 -7.2517 v ǁVelocityǁ 0.0094697 29.746 15.156 20.137 v Pressure -313.43 448.78 186.47 186.21 v k 0.0064634 9.3424 1.0336 0.72283 v omega 93.789 6.8747e+05 11466 694.18 v TurbVisc 8.4731e-08 0.010556 0.00090563 0.0012507 v CourantNb 0.0026022 1.0402 0.93968 0.99858 v FourierNb 0.0056327 10 2.8035 0.32667 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1238e-05 0.0081777 0.0006233 0.00049054 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0021 11.022 3.7432 1.3253 INSTANT 0.266000000E-02 TIME STEP NUMBER 266 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499910E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35188E-01 0.36341E+02 Friction velocity uk : 0.44034E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10729E+03 6 0.47398E-03 0.47433E+00 0.16996E+01 c Velocity[X] 0.19752E+00 c Velocity[Y] 0.81071E-01 c Velocity[Z] 0.19574E+00 c Pressure 0.82587E-03 10 0.39647E-04 0.11665E-01 0.33833E+00 c k 0.33398E+01 5 0.27390E-05 0.28998E-01 0.74550E+01 c omega 0.27200E+05 3 0.78734E-06 0.11715E+05 0.81686E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.014 24.601 -4.4382 -6.0615 v Velocity[Y] -24.378 26.999 0.85989 1.1685 v Velocity[Z] -26.975 21.051 -5.3458 -7.2517 v ǁVelocityǁ 0.0091451 29.744 15.157 20.137 v Pressure -312.96 448.7 186.47 186.21 v k 0.0064688 9.3606 1.0339 0.72363 v omega 93.636 6.8747e+05 11467 693.9 v TurbVisc 8.4743e-08 0.010556 0.00090737 0.0012543 v CourantNb 0.0025504 1.0361 0.93969 0.99858 v FourierNb 0.0056426 10 2.8033 0.32676 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1234e-05 0.0081263 0.00062327 0.00049053 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0025 11.03 3.743 1.3253 INSTANT 0.267000000E-02 TIME STEP NUMBER 267 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500128E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62215E-01 0.36312E+02 Friction velocity uk : 0.44053E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10729E+03 6 0.47701E-03 0.47147E+00 0.16947E+01 c Velocity[X] 0.19640E+00 c Velocity[Y] 0.80165E-01 c Velocity[Z] 0.19490E+00 c Pressure 0.83146E-03 11 0.41237E-04 0.11744E-01 0.38534E+00 c k 0.33438E+01 5 0.27075E-05 0.28698E-01 0.74152E+01 c omega 0.27206E+05 3 0.78193E-06 0.11545E+05 0.81052E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.997 24.545 -4.4381 -6.0614 v Velocity[Y] -24.389 26.995 0.85993 1.1685 v Velocity[Z] -26.973 21.016 -5.3459 -7.2517 v ǁVelocityǁ 0.0088199 29.731 15.158 20.137 v Pressure -313.18 448.62 186.46 186.2 v k 0.0064743 9.3735 1.0342 0.72443 v omega 93.491 6.8747e+05 11468 693.62 v TurbVisc 8.4743e-08 0.010556 0.0009091 0.001258 v CourantNb 0.0025679 1.0356 0.93969 0.99858 v FourierNb 0.0056525 10 2.803 0.32684 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.123e-05 0.0081313 0.00062324 0.00049053 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0024 11.02 3.7427 1.3254 INSTANT 0.268000000E-02 TIME STEP NUMBER 268 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500333E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60828E-01 0.36266E+02 Friction velocity uk : 0.44072E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10730E+03 6 0.47459E-03 0.46790E+00 0.16891E+01 c Velocity[X] 0.19534E+00 c Velocity[Y] 0.79094E-01 c Velocity[Z] 0.19347E+00 c Pressure 0.82775E-03 13 0.38625E-04 0.11691E-01 0.43965E+00 c k 0.33478E+01 5 0.26999E-05 0.28407E-01 0.73760E+01 c omega 0.27211E+05 3 0.78501E-06 0.11560E+05 0.80982E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.007 24.521 -4.438 -6.0614 v Velocity[Y] -24.388 26.992 0.85998 1.1685 v Velocity[Z] -26.971 20.972 -5.3459 -7.2517 v ǁVelocityǁ 0.010144 29.739 15.158 20.137 v Pressure -313.26 448.54 186.44 186.18 v k 0.0064793 9.3907 1.0345 0.72524 v omega 93.334 6.8747e+05 11469 693.34 v TurbVisc 8.474e-08 0.010556 0.00091083 0.0012616 v CourantNb 0.0024773 1.0377 0.93969 0.99858 v FourierNb 0.0056624 10 2.8027 0.32692 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1226e-05 0.0082208 0.00062321 0.00049053 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0032 11.034 3.7424 1.3255 INSTANT 0.269000000E-02 TIME STEP NUMBER 269 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500471E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36571E-01 0.36348E+02 Friction velocity uk : 0.44088E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10730E+03 6 0.48761E-03 0.46572E+00 0.16854E+01 c Velocity[X] 0.19442E+00 c Velocity[Y] 0.78731E-01 c Velocity[Z] 0.19256E+00 c Pressure 0.83351E-03 25 0.40393E-04 0.11773E-01 0.61650E+01 c k 0.33517E+01 5 0.26744E-05 0.28116E-01 0.73369E+01 c omega 0.27217E+05 3 0.77650E-06 0.11394E+05 0.80333E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.013 24.493 -4.4379 -6.0615 v Velocity[Y] -24.403 26.989 0.86002 1.1685 v Velocity[Z] -26.968 20.921 -5.346 -7.2517 v ǁVelocityǁ 0.0093452 29.742 15.159 20.137 v Pressure -313.17 447.96 185.93 185.67 v k 0.0064855 9.4025 1.0348 0.72605 v omega 93.18 6.8747e+05 11469 693.07 v TurbVisc 8.4741e-08 0.010556 0.00091255 0.0012653 v CourantNb 0.0027188 1.0386 0.9397 0.99858 v FourierNb 0.0056723 10 2.8025 0.32701 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1222e-05 0.0083716 0.00062318 0.00049052 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.003 11.019 3.7422 1.3256 INSTANT 0.270000000E-02 TIME STEP NUMBER 270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500165E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62846E-01 0.36249E+02 Friction velocity uk : 0.44110E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10731E+03 6 0.48335E-03 0.46381E+00 0.16852E+01 c Velocity[X] 0.19393E+00 c Velocity[Y] 0.78220E-01 c Velocity[Z] 0.19167E+00 c Pressure 0.84415E-03 12 0.40214E-04 0.11923E-01 0.39500E+00 c k 0.33557E+01 5 0.26651E-05 0.27828E-01 0.72978E+01 c omega 0.27223E+05 3 0.77987E-06 0.11373E+05 0.80210E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.014 24.466 -4.4378 -6.0615 v Velocity[Y] -24.411 26.985 0.86007 1.1685 v Velocity[Z] -26.958 20.861 -5.346 -7.2517 v ǁVelocityǁ 0.008805 29.745 15.16 20.137 v Pressure -313.35 447.81 185.93 185.67 v k 0.006491 9.4123 1.0351 0.72686 v omega 93.032 6.8747e+05 11470 692.8 v TurbVisc 8.4754e-08 0.010556 0.00091427 0.0012689 v CourantNb 0.0024982 1.0381 0.9397 0.99858 v FourierNb 0.0056822 10 2.8023 0.32709 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1218e-05 0.008468 0.00062315 0.00049052 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0033 11.022 3.742 1.3257 INSTANT 0.271000000E-02 TIME STEP NUMBER 271 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499924E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60799E-01 0.36360E+02 Friction velocity uk : 0.44128E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10731E+03 6 0.47453E-03 0.46009E+00 0.16760E+01 c Velocity[X] 0.19259E+00 c Velocity[Y] 0.76855E-01 c Velocity[Z] 0.19064E+00 c Pressure 0.83010E-03 13 0.40507E-04 0.11724E-01 0.48926E+00 c k 0.33597E+01 5 0.26146E-05 0.27541E-01 0.72587E+01 c omega 0.27229E+05 3 0.76509E-06 0.11351E+05 0.80110E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.016 24.446 -4.4377 -6.0615 v Velocity[Y] -24.425 26.981 0.86011 1.1685 v Velocity[Z] -26.95 20.796 -5.3461 -7.2517 v ǁVelocityǁ 0.01037 29.732 15.161 20.137 v Pressure -313.49 447.79 185.94 185.68 v k 0.0064971 9.4289 1.0354 0.72767 v omega 92.883 6.8747e+05 11471 692.54 v TurbVisc 8.476e-08 0.010556 0.00091598 0.0012725 v CourantNb 0.002567 1.0409 0.9397 0.99858 v FourierNb 0.0056921 10 2.802 0.32718 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1214e-05 0.0086042 0.00062312 0.00049052 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0037 11.017 3.7417 1.3258 INSTANT 0.272000000E-02 TIME STEP NUMBER 272 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499729E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70807E-01 0.36330E+02 Friction velocity uk : 0.44149E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10732E+03 6 0.47820E-03 0.45684E+00 0.16704E+01 c Velocity[X] 0.19135E+00 c Velocity[Y] 0.76237E-01 c Velocity[Z] 0.18925E+00 c Pressure 0.82754E-03 19 0.38325E-04 0.11688E-01 0.31381E+01 c k 0.33637E+01 5 0.25898E-05 0.27255E-01 0.72195E+01 c omega 0.27234E+05 3 0.76190E-06 0.11274E+05 0.79712E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.022 24.394 -4.4376 -6.0614 v Velocity[Y] -24.439 26.977 0.86015 1.1685 v Velocity[Z] -26.945 20.721 -5.3461 -7.2516 v ǁVelocityǁ 0.0092541 29.737 15.161 20.137 v Pressure -312.59 447.45 186.05 185.78 v k 0.0065031 9.4399 1.0358 0.72848 v omega 92.729 6.8747e+05 11472 692.28 v TurbVisc 8.4766e-08 0.010556 0.00091768 0.001276 v CourantNb 0.0023835 1.044 0.93971 0.99858 v FourierNb 0.005702 10 2.8018 0.32727 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.121e-05 0.0087821 0.00062308 0.00049051 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0034 11.044 3.7415 1.3258 INSTANT 0.273000000E-02 TIME STEP NUMBER 273 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499757E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63886E-01 0.36232E+02 Friction velocity uk : 0.44169E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10733E+03 6 0.47925E-03 0.45471E+00 0.16672E+01 c Velocity[X] 0.19089E+00 c Velocity[Y] 0.75612E-01 c Velocity[Z] 0.18821E+00 c Pressure 0.82461E-03 18 0.39495E-04 0.11647E-01 0.34968E+01 c k 0.33676E+01 5 0.25521E-05 0.26974E-01 0.71807E+01 c omega 0.27240E+05 3 0.76313E-06 0.11189E+05 0.79394E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.012 24.398 -4.4375 -6.0614 v Velocity[Y] -24.437 26.973 0.8602 1.1685 v Velocity[Z] -26.94 20.685 -5.3462 -7.2516 v ǁVelocityǁ 0.0084996 29.746 15.162 20.138 v Pressure -312.81 448.06 186.29 186.02 v k 0.0065093 9.4494 1.0361 0.7293 v omega 92.584 6.8747e+05 11473 692.02 v TurbVisc 8.4766e-08 0.010556 0.00091937 0.0012796 v CourantNb 0.0024656 1.045 0.93971 0.99858 v FourierNb 0.005712 10 2.8016 0.32735 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1206e-05 0.0089019 0.00062305 0.00049051 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0036 11.027 3.7413 1.3259 INSTANT 0.274000000E-02 TIME STEP NUMBER 274 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499811E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40539E-01 0.36324E+02 Friction velocity uk : 0.44190E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10733E+03 6 0.47991E-03 0.45207E+00 0.16614E+01 c Velocity[X] 0.18981E+00 c Velocity[Y] 0.74810E-01 c Velocity[Z] 0.18745E+00 c Pressure 0.83364E-03 13 0.39260E-04 0.11775E-01 0.57110E+00 c k 0.33716E+01 5 0.25438E-05 0.26695E-01 0.71421E+01 c omega 0.27245E+05 3 0.76069E-06 0.11177E+05 0.79238E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.998 24.348 -4.4374 -6.0614 v Velocity[Y] -24.449 26.969 0.86025 1.1685 v Velocity[Z] -26.933 20.641 -5.3462 -7.2516 v ǁVelocityǁ 0.0087174 29.742 15.163 20.138 v Pressure -312.93 448.24 186.32 186.06 v k 0.0065138 9.4664 1.0364 0.73012 v omega 92.448 6.8747e+05 11474 691.76 v TurbVisc 8.477e-08 0.010556 0.00092105 0.0012831 v CourantNb 0.0024485 1.045 0.93971 0.99858 v FourierNb 0.0057219 10 2.8014 0.32744 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1202e-05 0.0089917 0.00062302 0.00049051 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0036 11.016 3.7411 1.326 INSTANT 0.275000000E-02 TIME STEP NUMBER 275 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499865E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43332E-01 0.36318E+02 Friction velocity uk : 0.44206E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10734E+03 6 0.47931E-03 0.44943E+00 0.16578E+01 c Velocity[X] 0.18866E+00 c Velocity[Y] 0.74075E-01 c Velocity[Z] 0.18669E+00 c Pressure 0.84062E-03 13 0.38916E-04 0.11873E-01 0.51897E+00 c k 0.33756E+01 5 0.25023E-05 0.26418E-01 0.71034E+01 c omega 0.27251E+05 3 0.74855E-06 0.10958E+05 0.78502E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.007 24.343 -4.4373 -6.0614 v Velocity[Y] -24.455 26.964 0.86029 1.1685 v Velocity[Z] -26.929 20.593 -5.3463 -7.2516 v ǁVelocityǁ 0.010393 29.727 15.164 20.138 v Pressure -312.13 448.28 186.35 186.08 v k 0.006519 9.4767 1.0367 0.73093 v omega 92.306 6.8747e+05 11474 691.51 v TurbVisc 8.4776e-08 0.010556 0.00092273 0.0012867 v CourantNb 0.0025584 1.0469 0.93972 0.99858 v FourierNb 0.0057319 10 2.8012 0.32753 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1198e-05 0.0091616 0.00062299 0.00049051 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0039 11.027 3.7409 1.3261 INSTANT 0.276000000E-02 TIME STEP NUMBER 276 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499884E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25612E-01 0.36209E+02 Friction velocity uk : 0.44223E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10734E+03 6 0.47762E-03 0.44731E+00 0.16533E+01 c Velocity[X] 0.18810E+00 c Velocity[Y] 0.73434E-01 c Velocity[Z] 0.18578E+00 c Pressure 0.84013E-03 13 0.38280E-04 0.11866E-01 0.66661E+00 c k 0.33796E+01 5 0.24726E-05 0.26144E-01 0.70650E+01 c omega 0.27256E+05 3 0.74523E-06 0.11005E+05 0.78572E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.008 24.293 -4.4372 -6.0614 v Velocity[Y] -24.469 26.957 0.86034 1.1685 v Velocity[Z] -26.926 20.537 -5.3463 -7.2516 v ǁVelocityǁ 0.0089693 29.737 15.164 20.138 v Pressure -312.51 448.44 186.39 186.12 v k 0.0065241 9.4866 1.037 0.73175 v omega 92.148 6.8747e+05 11475 691.27 v TurbVisc 8.4783e-08 0.010556 0.00092439 0.0012902 v CourantNb 0.0023741 1.0575 0.93972 0.99858 v FourierNb 0.0057419 10 2.801 0.32762 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1194e-05 0.0092157 0.00062296 0.0004905 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.004 11.023 3.7407 1.3262 INSTANT 0.277000000E-02 TIME STEP NUMBER 277 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499850E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54937E-01 0.36307E+02 Friction velocity uk : 0.44241E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10735E+03 6 0.47974E-03 0.44437E+00 0.16486E+01 c Velocity[X] 0.18719E+00 c Velocity[Y] 0.72610E-01 c Velocity[Z] 0.18457E+00 c Pressure 0.82644E-03 24 0.37678E-04 0.11673E-01 0.77822E+01 c k 0.33836E+01 5 0.24714E-05 0.25871E-01 0.70265E+01 c omega 0.27262E+05 3 0.74593E-06 0.10846E+05 0.77949E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.015 24.266 -4.4371 -6.0614 v Velocity[Y] -24.469 26.95 0.86038 1.1685 v Velocity[Z] -26.925 20.476 -5.3463 -7.2516 v ǁVelocityǁ 0.010096 29.738 15.165 20.138 v Pressure -312.01 449.42 187.02 186.75 v k 0.0065303 9.5048 1.0374 0.73257 v omega 91.996 6.8747e+05 11476 691.02 v TurbVisc 8.478e-08 0.010556 0.00092606 0.0012937 v CourantNb 0.0024566 1.0701 0.93973 0.99858 v FourierNb 0.0057518 10 2.8008 0.32771 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1191e-05 0.009325 0.00062293 0.0004905 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0042 11.022 3.7405 1.3263 INSTANT 0.278000000E-02 TIME STEP NUMBER 278 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499858E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69581E-01 0.36262E+02 Friction velocity uk : 0.44261E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10735E+03 6 0.48037E-03 0.44183E+00 0.16442E+01 c Velocity[X] 0.18642E+00 c Velocity[Y] 0.72188E-01 c Velocity[Z] 0.18322E+00 c Pressure 0.82804E-03 10 0.37478E-04 0.11695E-01 0.33360E+00 c k 0.33875E+01 5 0.24310E-05 0.25602E-01 0.69884E+01 c omega 0.27267E+05 3 0.73997E-06 0.10823E+05 0.77784E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.019 24.271 -4.437 -6.0614 v Velocity[Y] -24.481 26.944 0.86043 1.1685 v Velocity[Z] -26.918 20.408 -5.3464 -7.2516 v ǁVelocityǁ 0.0089388 29.739 15.166 20.138 v Pressure -311.77 449.41 187.01 186.75 v k 0.0065359 9.5164 1.0377 0.7334 v omega 91.855 6.8747e+05 11477 690.78 v TurbVisc 8.4779e-08 0.010556 0.00092772 0.0012971 v CourantNb 0.0025317 1.0597 0.93973 0.99858 v FourierNb 0.0057618 10 2.8006 0.3278 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1187e-05 0.0094955 0.0006229 0.0004905 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0041 11.012 3.7403 1.3264 INSTANT 0.279000000E-02 TIME STEP NUMBER 279 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499965E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60725E-01 0.36221E+02 Friction velocity uk : 0.44281E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10736E+03 6 0.48008E-03 0.44038E+00 0.16414E+01 c Velocity[X] 0.18553E+00 c Velocity[Y] 0.71761E-01 c Velocity[Z] 0.18309E+00 c Pressure 0.83464E-03 13 0.38418E-04 0.11789E-01 0.43311E+00 c k 0.33915E+01 5 0.24329E-05 0.25337E-01 0.69505E+01 c omega 0.27273E+05 3 0.74340E-06 0.10734E+05 0.77471E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.995 24.222 -4.4369 -6.0614 v Velocity[Y] -24.486 26.94 0.86048 1.1685 v Velocity[Z] -26.915 20.331 -5.3464 -7.2516 v ǁVelocityǁ 0.0089183 29.723 15.167 20.138 v Pressure -311.74 449.39 187 186.74 v k 0.0065424 9.5346 1.038 0.73422 v omega 91.712 6.8747e+05 11478 690.54 v TurbVisc 8.4782e-08 0.010556 0.00092938 0.0013006 v CourantNb 0.0024219 1.0546 0.93973 0.99858 v FourierNb 0.0057718 10 2.8004 0.32789 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1183e-05 0.0095706 0.00062287 0.00049049 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0043 11.032 3.7401 1.3265 INSTANT 0.280000000E-02 TIME STEP NUMBER 280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500112E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60741E-01 0.36274E+02 Friction velocity uk : 0.44303E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10736E+03 6 0.48057E-03 0.43753E+00 0.16361E+01 c Velocity[X] 0.18451E+00 c Velocity[Y] 0.70740E-01 c Velocity[Z] 0.18228E+00 c Pressure 0.82953E-03 19 0.36501E-04 0.11717E-01 0.39485E+01 c k 0.33955E+01 5 0.24067E-05 0.25080E-01 0.69136E+01 c omega 0.27279E+05 3 0.73658E-06 0.10844E+05 0.77679E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.003 24.198 -4.4367 -6.0614 v Velocity[Y] -24.494 26.936 0.86053 1.1685 v Velocity[Z] -26.914 20.25 -5.3465 -7.2516 v ǁVelocityǁ 0.010088 29.727 15.167 20.138 v Pressure -311.91 448.89 186.74 186.47 v k 0.0065448 9.5475 1.0384 0.73504 v omega 91.565 6.8747e+05 11478 690.31 v TurbVisc 8.4795e-08 0.010556 0.00093104 0.0013041 v CourantNb 0.0024401 1.0544 0.93974 0.99858 v FourierNb 0.0057818 10 2.8002 0.32798 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1179e-05 0.0095848 0.00062284 0.00049049 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044 11.026 3.7399 1.3266 INSTANT 0.281000000E-02 TIME STEP NUMBER 281 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500185E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49684E-01 0.36298E+02 Friction velocity uk : 0.44311E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10737E+03 6 0.48027E-03 0.43524E+00 0.16323E+01 c Velocity[X] 0.18391E+00 c Velocity[Y] 0.70184E-01 c Velocity[Z] 0.18115E+00 c Pressure 0.82429E-03 11 0.36699E-04 0.11643E-01 0.39638E+00 c k 0.33995E+01 5 0.24032E-05 0.24818E-01 0.68759E+01 c omega 0.27284E+05 3 0.73198E-06 0.10626E+05 0.76876E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.009 24.203 -4.4366 -6.0614 v Velocity[Y] -24.499 26.932 0.86058 1.1685 v Velocity[Z] -26.912 20.167 -5.3465 -7.2516 v ǁVelocityǁ 0.010997 29.732 15.168 20.138 v Pressure -311.42 448.87 186.73 186.46 v k 0.006547 9.5651 1.0387 0.73587 v omega 91.42 6.8747e+05 11479 690.07 v TurbVisc 8.4797e-08 0.010556 0.00093269 0.0013076 v CourantNb 0.0025476 1.0514 0.93974 0.99858 v FourierNb 0.0057917 10 2.8 0.32807 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1175e-05 0.0097963 0.00062281 0.00049049 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044 11.019 3.7398 1.3267 INSTANT 0.282000000E-02 TIME STEP NUMBER 282 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500200E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75396E-01 0.36190E+02 Friction velocity uk : 0.44318E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10737E+03 6 0.47549E-03 0.43254E+00 0.16264E+01 c Velocity[X] 0.18331E+00 c Velocity[Y] 0.69409E-01 c Velocity[Z] 0.17982E+00 c Pressure 0.81835E-03 17 0.36758E-04 0.11559E-01 0.15903E+01 c k 0.34035E+01 5 0.23464E-05 0.24557E-01 0.68381E+01 c omega 0.27290E+05 3 0.71813E-06 0.10533E+05 0.76498E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.009 24.157 -4.4365 -6.0614 v Velocity[Y] -24.509 26.928 0.86063 1.1685 v Velocity[Z] -26.905 20.078 -5.3466 -7.2516 v ǁVelocityǁ 0.0088774 29.729 15.169 20.138 v Pressure -311.61 448.97 186.67 186.4 v k 0.0065481 9.5781 1.0391 0.7367 v omega 91.272 6.8747e+05 11480 689.85 v TurbVisc 8.4798e-08 0.010556 0.00093435 0.0013111 v CourantNb 0.0022121 1.044 0.93975 0.99858 v FourierNb 0.0058018 10 2.7998 0.32817 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1171e-05 0.0097232 0.00062278 0.00049049 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044 11.023 3.7396 1.3267 INSTANT 0.283000000E-02 TIME STEP NUMBER 283 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500069E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59929E-01 0.36276E+02 Friction velocity uk : 0.44322E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10738E+03 5 0.47716E-03 0.42992E+00 0.16233E+01 c Velocity[X] 0.18218E+00 c Velocity[Y] 0.68676E-01 c Velocity[Z] 0.17907E+00 c Pressure 0.81114E-03 11 0.37362E-04 0.11457E-01 0.32978E+00 c k 0.34075E+01 5 0.23418E-05 0.24305E-01 0.68013E+01 c omega 0.27295E+05 3 0.72185E-06 0.10489E+05 0.76314E+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 k a omega a Local Time Step ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.014 24.165 -4.4364 -6.0614 v Velocity[Y] -24.508 26.924 0.86068 1.1685 v Velocity[Z] -26.902 19.988 -5.3466 -7.2516 v ǁVelocityǁ 0.010327 29.712 15.169 20.138 v Pressure -311.75 448.96 186.67 186.4 v k 0.0065489 9.5972 1.0394 0.73752 v omega 91.136 6.8747e+05 11481 689.62 v TurbVisc 8.4787e-08 0.010556 0.00093601 0.0013145 v CourantNb 0.0023652 1.0378 0.93975 0.99858 v FourierNb 0.0058117 10 2.7997 0.32826 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1167e-05 0.0099246 0.00062275 0.00049048 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0045 11.012 3.7394 1.3268 INSTANT 0.284000000E-02 TIME STEP NUMBER 284 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499990E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46058E-01 0.36240E+02 Friction velocity uk : 0.44325E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10738E+03 6 0.48199E-03 0.42872E+00 0.16193E+01 c Velocity[X] 0.18172E+00 c Velocity[Y] 0.68543E-01 c Velocity[Z] 0.17845E+00 c Pressure 0.82521E-03 13 0.36690E-04 0.11656E-01 0.35086E+00 c k 0.34115E+01 5 0.23186E-05 0.24058E-01 0.67650E+01 c omega 0.27301E+05 3 0.71297E-06 0.10428E+05 0.75992E+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 k a omega a Local Time Step 0.010001 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.019 24.147 -4.4363 -6.0614 v Velocity[Y] -24.522 26.921 0.86073 1.1685 v Velocity[Z] -26.9 19.894 -5.3466 -7.2516 v ǁVelocityǁ 0.010425 29.718 15.17 20.138 v Pressure -311.02 449.03 186.67 186.4 v k 0.0065487 9.6127 1.0398 0.73835 v omega 91.008 6.8747e+05 11482 689.4 v TurbVisc 8.4782e-08 0.010556 0.00093766 0.001318 v CourantNb 0.0024162 1.0459 0.93975 0.99858 v FourierNb 0.0058218 10 2.7995 0.32836 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1163e-05 0.01 0.00062272 0.00049048 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0045 11.033 3.7393 1.3269 INSTANT 0.285000000E-02 TIME STEP NUMBER 285 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499895E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56318E-01 0.36186E+02 Friction velocity uk : 0.44324E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10739E+03 5 0.48083E-03 0.42708E+00 0.16176E+01 c Velocity[X] 0.18122E+00 c Velocity[Y] 0.67754E-01 c Velocity[Z] 0.17810E+00 c Pressure 0.82826E-03 17 0.36797E-04 0.11699E-01 0.12708E+01 c k 0.34155E+01 5 0.23278E-05 0.23813E-01 0.67288E+01 c omega 0.27306E+05 3 0.71893E-06 0.10371E+05 0.75793E+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 k a omega a Local Time Step 0.010237 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.001 24.099 -4.4362 -6.0614 v Velocity[Y] -24.522 26.918 0.86078 1.1685 v Velocity[Z] -26.899 19.8 -5.3467 -7.2516 v ǁVelocityǁ 0.0093412 29.72 15.171 20.138 v Pressure -311.08 448.92 186.73 186.45 v k 0.0065486 9.6317 1.0401 0.73918 v omega 90.877 6.8747e+05 11483 689.18 v TurbVisc 8.4772e-08 0.010556 0.00093931 0.0013215 v CourantNb 0.0023666 1.0569 0.93976 0.99858 v FourierNb 0.0058317 10 2.7994 0.32845 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.116e-05 0.01 0.00062269 0.00049048 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044 11.055 3.7391 1.327 INSTANT 0.286000000E-02 TIME STEP NUMBER 286 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499784E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16679E-01 0.36256E+02 Friction velocity uk : 0.44324E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10739E+03 5 0.47129E-03 0.42379E+00 0.16103E+01 c Velocity[X] 0.18024E+00 c Velocity[Y] 0.67031E-01 c Velocity[Z] 0.17652E+00 c Pressure 0.82434E-03 10 0.36021E-04 0.11643E-01 0.35528E+00 c k 0.34195E+01 5 0.23011E-05 0.23566E-01 0.66923E+01 c omega 0.27312E+05 3 0.71023E-06 0.10370E+05 0.75706E+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 k a omega a Local Time Step 0.010229 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.998 24.104 -4.4361 -6.0614 v Velocity[Y] -24.537 26.915 0.86083 1.1685 v Velocity[Z] -26.891 19.7 -5.3467 -7.2516 v ǁVelocityǁ 0.010074 29.719 15.172 20.139 v Pressure -311.09 449.04 186.74 186.47 v k 0.0065489 9.6477 1.0405 0.74001 v omega 90.746 6.8747e+05 11484 688.96 v TurbVisc 8.4773e-08 0.010556 0.00094097 0.001325 v CourantNb 0.0022647 1.0478 0.93976 0.99858 v FourierNb 0.0058417 10 2.7992 0.32855 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1156e-05 0.01 0.00062266 0.00049048 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044 11.033 3.739 1.3271 INSTANT 0.287000000E-02 TIME STEP NUMBER 287 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499670E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49158E-01 0.36201E+02 Friction velocity uk : 0.44325E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10740E+03 5 0.48001E-03 0.42151E+00 0.16059E+01 c Velocity[X] 0.17917E+00 c Velocity[Y] 0.66630E-01 c Velocity[Z] 0.17572E+00 c Pressure 0.81597E-03 24 0.35858E-04 0.11525E-01 0.93820E+01 c k 0.34235E+01 5 0.22764E-05 0.23323E-01 0.66561E+01 c omega 0.27317E+05 3 0.70283E-06 0.10224E+05 0.75107E+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 k a omega a Local Time Step 0.010652 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.003 24.088 -4.436 -6.0614 v Velocity[Y] -24.537 26.911 0.86089 1.1685 v Velocity[Z] -26.889 19.601 -5.3468 -7.2516 v ǁVelocityǁ 0.010706 29.703 15.172 20.139 v Pressure -310.17 450.01 187.53 187.25 v k 0.0065496 9.6665 1.0408 0.74084 v omega 90.615 6.8747e+05 11484 688.75 v TurbVisc 8.4777e-08 0.010556 0.00094262 0.0013285 v CourantNb 0.0024483 1.0438 0.93977 0.99858 v FourierNb 0.0058517 10 2.799 0.32865 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1152e-05 0.01 0.00062263 0.00049048 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0045 11.031 3.7388 1.3272 INSTANT 0.288000000E-02 TIME STEP NUMBER 288 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499912E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39520E-01 0.36244E+02 Friction velocity uk : 0.44327E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10740E+03 5 0.48677E-03 0.41978E+00 0.16036E+01 c Velocity[X] 0.17866E+00 c Velocity[Y] 0.66137E-01 c Velocity[Z] 0.17499E+00 c Pressure 0.81671E-03 11 0.35980E-04 0.11536E-01 0.34914E+00 c k 0.34275E+01 5 0.22573E-05 0.23084E-01 0.66203E+01 c omega 0.27323E+05 3 0.70107E-06 0.10178E+05 0.74920E+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 k a omega a Local Time Step 0.010688 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.009 24.041 -4.4359 -6.0614 v Velocity[Y] -24.549 26.908 0.86094 1.1685 v Velocity[Z] -26.888 19.502 -5.3468 -7.2516 v ǁVelocityǁ 0.0089793 29.708 15.173 20.139 v Pressure -310.14 450.03 187.52 187.25 v k 0.0065502 9.6817 1.0412 0.74168 v omega 90.481 6.8747e+05 11485 688.53 v TurbVisc 8.4784e-08 0.010556 0.00094427 0.0013319 v CourantNb 0.0023742 1.0419 0.93977 0.99858 v FourierNb 0.0058617 10 2.7989 0.32874 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1148e-05 0.01 0.0006226 0.00049047 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0045 11.024 3.7387 1.3273 INSTANT 0.289000000E-02 TIME STEP NUMBER 289 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500154E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61836E-01 0.36223E+02 Friction velocity uk : 0.44329E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10741E+03 5 0.47737E-03 0.41773E+00 0.16005E+01 c Velocity[X] 0.17779E+00 c Velocity[Y] 0.65552E-01 c Velocity[Z] 0.17439E+00 c Pressure 0.82175E-03 18 0.36119E-04 0.11607E-01 0.89381E+00 c k 0.34315E+01 5 0.22491E-05 0.22853E-01 0.65853E+01 c omega 0.27328E+05 3 0.69828E-06 0.10191E+05 0.74895E+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 k a omega a Local Time Step 0.010852 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.015 24.052 -4.4358 -6.0614 v Velocity[Y] -24.546 26.905 0.86099 1.1685 v Velocity[Z] -26.886 19.406 -5.3469 -7.2516 v ǁVelocityǁ 0.011185 29.711 15.174 20.139 v Pressure -310.41 450.03 187.49 187.22 v k 0.0065515 9.7018 1.0416 0.74251 v omega 90.35 6.8747e+05 11486 688.32 v TurbVisc 8.4787e-08 0.010556 0.00094593 0.0013354 v CourantNb 0.0023888 1.0489 0.93978 0.99858 v FourierNb 0.0058717 10 2.7988 0.32884 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1144e-05 0.01 0.00062257 0.00049047 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0046 11.027 3.7385 1.3274 INSTANT 0.290000000E-02 TIME STEP NUMBER 290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500247E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63505E-01 0.36213E+02 Friction velocity uk : 0.44334E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10741E+03 5 0.47898E-03 0.41535E+00 0.15950E+01 c Velocity[X] 0.17699E+00 c Velocity[Y] 0.65064E-01 c Velocity[Z] 0.17329E+00 c Pressure 0.82717E-03 10 0.35567E-04 0.11683E-01 0.32671E+00 c k 0.34355E+01 5 0.22310E-05 0.22621E-01 0.65503E+01 c omega 0.27334E+05 3 0.69050E-06 0.99643E+04 0.74030E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.997 24.034 -4.4357 -6.0614 v Velocity[Y] -24.559 26.902 0.86104 1.1685 v Velocity[Z] -26.878 19.307 -5.3469 -7.2516 v ǁVelocityǁ 0.01024 29.708 15.175 20.139 v Pressure -309.95 450.14 187.48 187.21 v k 0.0065535 9.7173 1.0419 0.74335 v omega 90.224 6.8747e+05 11487 688.12 v TurbVisc 8.4798e-08 0.010556 0.00094758 0.0013389 v CourantNb 0.0022922 1.047 0.93978 0.99858 v FourierNb 0.0058817 10 2.7986 0.32894 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1141e-05 0.01 0.00062254 0.00049047 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0046 11.01 3.7384 1.3275 INSTANT 0.291000000E-02 TIME STEP NUMBER 291 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500283E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69926E-01 0.36219E+02 Friction velocity uk : 0.44340E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10742E+03 5 0.48368E-03 0.41338E+00 0.15917E+01 c Velocity[X] 0.17623E+00 c Velocity[Y] 0.64558E-01 c Velocity[Z] 0.17259E+00 c Pressure 0.81948E-03 10 0.36202E-04 0.11575E-01 0.33115E+00 c k 0.34395E+01 5 0.22435E-05 0.22396E-01 0.65158E+01 c omega 0.27340E+05 3 0.70448E-06 0.99860E+04 0.74080E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.008 23.99 -4.4356 -6.0614 v Velocity[Y] -24.556 26.898 0.8611 1.1685 v Velocity[Z] -26.875 19.212 -5.3469 -7.2516 v ǁVelocityǁ 0.0094848 29.692 15.175 20.139 v Pressure -310.12 450.07 187.48 187.2 v k 0.0065561 9.7354 1.0423 0.74418 v omega 90.094 6.8747e+05 11488 687.92 v TurbVisc 8.4808e-08 0.010556 0.00094923 0.0013424 v CourantNb 0.0021636 1.0486 0.93978 0.99858 v FourierNb 0.0058916 10 2.7985 0.32904 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1137e-05 0.01 0.00062251 0.00049047 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0046 11.021 3.7383 1.3276 INSTANT 0.292000000E-02 TIME STEP NUMBER 292 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500280E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65490E-01 0.36224E+02 Friction velocity uk : 0.44349E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10742E+03 5 0.48372E-03 0.41152E+00 0.15874E+01 c Velocity[X] 0.17552E+00 c Velocity[Y] 0.63876E-01 c Velocity[Z] 0.17213E+00 c Pressure 0.81896E-03 13 0.35813E-04 0.11568E-01 0.48523E+00 c k 0.34436E+01 5 0.21891E-05 0.22173E-01 0.64817E+01 c omega 0.27345E+05 3 0.68393E-06 0.10040E+05 0.74180E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.011 24.002 -4.4355 -6.0614 v Velocity[Y] -24.569 26.895 0.86115 1.1685 v Velocity[Z] -26.874 19.121 -5.347 -7.2516 v ǁVelocityǁ 0.01007 29.695 15.176 20.139 v Pressure -310.11 450.15 187.45 187.18 v k 0.0065588 9.751 1.0427 0.74502 v omega 89.957 6.8747e+05 11489 687.71 v TurbVisc 8.4821e-08 0.010556 0.00095088 0.0013458 v CourantNb 0.0023732 1.0436 0.93979 0.99858 v FourierNb 0.0059016 10 2.7983 0.32915 v total_pressure 1.0101e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1133e-05 0.01 0.00062249 0.00049047 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044 11.018 3.7381 1.3277 INSTANT 0.293000000E-02 TIME STEP NUMBER 293 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500247E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18531E-01 0.36177E+02 Friction velocity uk : 0.44358E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10743E+03 5 0.48617E-03 0.40969E+00 0.15861E+01 c Velocity[X] 0.17506E+00 c Velocity[Y] 0.63493E-01 c Velocity[Z] 0.17113E+00 c Pressure 0.82825E-03 17 0.35030E-04 0.11699E-01 0.19984E+01 c k 0.34476E+01 5 0.21732E-05 0.21955E-01 0.64481E+01 c omega 0.27351E+05 3 0.67773E-06 0.99352E+04 0.73732E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.008 23.989 -4.4354 -6.0614 v Velocity[Y] -24.564 26.892 0.86121 1.1685 v Velocity[Z] -26.872 19.033 -5.347 -7.2516 v ǁVelocityǁ 0.0092643 29.698 15.177 20.139 v Pressure -309.52 449.91 187.33 187.05 v k 0.0065622 9.77 1.043 0.74585 v omega 89.828 6.8747e+05 11490 687.52 v TurbVisc 8.4827e-08 0.010556 0.00095254 0.0013493 v CourantNb 0.0023173 1.0459 0.93979 0.99858 v FourierNb 0.0059115 10 2.7982 0.32925 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1129e-05 0.01 0.00062246 0.00049047 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0042 11.015 3.738 1.3278 INSTANT 0.294000000E-02 TIME STEP NUMBER 294 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162500090E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63482E-01 0.36165E+02 Friction velocity uk : 0.44370E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10743E+03 5 0.48046E-03 0.40806E+00 0.15820E+01 c Velocity[X] 0.17447E+00 c Velocity[Y] 0.63015E-01 c Velocity[Z] 0.17057E+00 c Pressure 0.83839E-03 10 0.34907E-04 0.11842E-01 0.36283E+00 c k 0.34516E+01 5 0.21535E-05 0.21739E-01 0.64146E+01 c omega 0.27356E+05 3 0.67295E-06 0.97637E+04 0.73126E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.013 23.944 -4.4353 -6.0614 v Velocity[Y] -24.579 26.889 0.86126 1.1685 v Velocity[Z] -26.865 18.947 -5.3471 -7.2516 v ǁVelocityǁ 0.010495 29.699 15.177 20.139 v Pressure -309.83 449.96 187.32 187.04 v k 0.0065657 9.7898 1.0434 0.74669 v omega 89.704 6.8747e+05 11490 687.32 v TurbVisc 8.4839e-08 0.010556 0.00095419 0.0013528 v CourantNb 0.0022504 1.0413 0.9398 0.99858 v FourierNb 0.0059215 10 2.7981 0.32935 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1126e-05 0.01 0.00062243 0.00049046 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044 11.023 3.7379 1.3279 INSTANT 0.295000000E-02 TIME STEP NUMBER 295 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499933E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55126E-01 0.36195E+02 Friction velocity uk : 0.44382E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10744E+03 5 0.47549E-03 0.40494E+00 0.15759E+01 c Velocity[X] 0.17315E+00 c Velocity[Y] 0.62209E-01 c Velocity[Z] 0.16958E+00 c Pressure 0.81091E-03 10 0.33431E-04 0.11454E-01 0.37932E+00 c k 0.34556E+01 5 0.21407E-05 0.21525E-01 0.63813E+01 c omega 0.27362E+05 3 0.67502E-06 0.97920E+04 0.73160E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.02 23.957 -4.4352 -6.0614 v Velocity[Y] -24.574 26.885 0.86132 1.1685 v Velocity[Z] -26.862 18.865 -5.3471 -7.2516 v ǁVelocityǁ 0.010381 29.678 15.178 20.139 v Pressure -309.8 449.83 187.33 187.05 v k 0.0065703 9.8022 1.0438 0.74753 v omega 89.564 6.8747e+05 11491 687.13 v TurbVisc 8.4848e-08 0.010556 0.00095584 0.0013563 v CourantNb 0.0022704 1.0373 0.9398 0.99858 v FourierNb 0.0059314 10 2.798 0.32946 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1122e-05 0.01 0.0006224 0.00049046 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0045 11.01 3.7378 1.328 INSTANT 0.296000000E-02 TIME STEP NUMBER 296 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499782E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38811E-01 0.36221E+02 Friction velocity uk : 0.44397E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10744E+03 5 0.48567E-03 0.40325E+00 0.15726E+01 c Velocity[X] 0.17234E+00 c Velocity[Y] 0.62072E-01 c Velocity[Z] 0.16884E+00 c Pressure 0.81188E-03 19 0.34671E-04 0.11468E-01 0.23354E+01 c k 0.34596E+01 5 0.21111E-05 0.21314E-01 0.63484E+01 c omega 0.27368E+05 3 0.66250E-06 0.97077E+04 0.72769E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.022 23.946 -4.4351 -6.0614 v Velocity[Y] -24.591 26.882 0.86138 1.1685 v Velocity[Z] -26.86 18.788 -5.3472 -7.2516 v ǁVelocityǁ 0.010088 29.686 15.179 20.139 v Pressure -309.05 449.85 187.45 187.18 v k 0.006575 9.8204 1.0442 0.74837 v omega 89.434 6.8747e+05 11492 686.93 v TurbVisc 8.4867e-08 0.010556 0.00095749 0.0013597 v CourantNb 0.0022866 1.0613 0.93981 0.99858 v FourierNb 0.0059413 10 2.7979 0.32956 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1118e-05 0.01 0.00062237 0.00049046 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0043 11.017 3.7377 1.3281 INSTANT 0.297000000E-02 TIME STEP NUMBER 297 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499867E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69506E-01 0.36135E+02 Friction velocity uk : 0.44413E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10744E+03 5 0.48834E-03 0.40224E+00 0.15715E+01 c Velocity[X] 0.17207E+00 c Velocity[Y] 0.61660E-01 c Velocity[Z] 0.16851E+00 c Pressure 0.82799E-03 10 0.33666E-04 0.11695E-01 0.34073E+00 c k 0.34637E+01 5 0.21244E-05 0.21110E-01 0.63163E+01 c omega 0.27373E+05 3 0.66998E-06 0.96922E+04 0.72705E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.998 23.902 -4.435 -6.0614 v Velocity[Y] -24.584 26.879 0.86143 1.1685 v Velocity[Z] -26.858 18.716 -5.3472 -7.2516 v ǁVelocityǁ 0.0094728 29.687 15.18 20.139 v Pressure -309 449.83 187.46 187.18 v k 0.0065794 9.8371 1.0446 0.74921 v omega 89.307 6.8747e+05 11493 686.75 v TurbVisc 8.4878e-08 0.010556 0.00095914 0.0013632 v CourantNb 0.002387 1.0539 0.93981 0.99858 v FourierNb 0.0059511 10 2.7977 0.32967 v total_pressure 1.0102e+05 1.0177e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1115e-05 0.01 0.00062234 0.00049046 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0047 11.018 3.7376 1.3283 Options set or changed by "control_file": ------------------------- max_time_step 298 (current: 298) Finished reading "control_file". INSTANT 0.298000000E-02 TIME STEP NUMBER 298 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 1365 -0.162500000E+01 Smooth wall 5 0 0.000000000E+00 Rough wall 6 191470 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1383 0.162499908E+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 ROUGH WALLS -------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64394E-01 0.36186E+02 Friction velocity uk : 0.44428E-01 0.18843E+00 Rough dimensionless dist yplus : 0.58195E-01 0.63559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 191470 ------------------------------------------------------------ Write final restart files checkpoint at iteration 298, Physical time 0.29800E-02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 298: checkpoint/main.csc End writing the options Wrote main variables to checkpoint: checkpoint/main.csc 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.csc End writing ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10745E+03 5 0.48784E-03 0.40003E+00 0.15672E+01 c Velocity[X] 0.17149E+00 c Velocity[Y] 0.60940E-01 c Velocity[Z] 0.16761E+00 c Pressure 0.82637E-03 20 0.34645E-04 0.11672E-01 0.51769E+01 c k 0.34677E+01 5 0.21017E-05 0.20906E-01 0.62842E+01 c omega 0.27379E+05 3 0.66661E-06 0.97095E+04 0.72719E+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 k a omega a Local Time Step 0.011 1 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.012 23.917 -4.4349 -6.0614 v Velocity[Y] -24.594 26.875 0.86149 1.1685 v Velocity[Z] -26.851 18.643 -5.3473 -7.2516 v ǁVelocityǁ 0.0093494 29.686 15.18 20.139 v Pressure -309.3 450.66 187.83 187.55 v k 0.006584 9.8553 1.0449 0.75006 v omega 89.172 6.8747e+05 11494 686.56 v TurbVisc 8.4882e-08 0.010556 0.00096079 0.0013667 v CourantNb 0.0021941 1.0531 0.93981 0.99858 v FourierNb 0.005961 10 2.7976 0.32977 v total_pressure 1.0102e+05 1.0178e+05 1.0151e+05 1.0151e+05 v Local Time Step 3.1111e-05 0.01 0.00062231 0.00049046 v Wall distance 4.6982e-05 0.12607 0.025498 0.049662 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 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 0.063559 0.06158 0.062214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044 11.013 3.7375 1.3284 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation