command: ./cs_solver *************************************************************** (R) Code_Saturne Version 6.0.5 Copyright (C) 1998-2019 EDF S.A., France revision 6.0.5-3e9e9e94c build sam. 21 nov. 2020 14:36:04 CET MPI version 3.1 (Open MPI 2.1.1) The Code_Saturne CFD tool is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 2 of the License, or (at your option) any later version. The Code_Saturne CFD tool is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. *************************************************************** Local case configuration: Date: mar. 05 janv. 2021 22:50:45 CET System: Linux 5.4.0-58-generic (Ubuntu 18.04.5 LTS) Machine: tsubasa-VirtualBox Processor: model name : Intel(R) Core(TM) i7-10610U CPU @ 1.80GHz Memory: 7962 MB User: tsubasa (tsubasa) Directory: /home/tsubasa/Desktop/sensecity/pipe2d/RESU/20210105-2250 OpenMP threads: 1 Processors/node: 1 I/O read method: standard input and output, serial access I/O write method: standard input and output, serial access External libraries for partitioning: ParMETIS 4.0.3 PT-SCOTCH 6.0.9 Reading metadata from file: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 4 (Nb variables ) NSCAL = 0 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) ----------------------------------------------------------- ** 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 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** STOKES ------ -- Continuous phase: ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old THETCP = -0.99900E+03 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculation ) ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. NTPABS = 0 (Initial time step) NTMABS = 500 (Final time step required) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 0 (Checkpoint frequency ) --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) -- -- -- --- run_solver.log files NTLIST = 1 (Output frequency ) -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted by the fluid on the boundary) ipstyp = 0 (y+ at boundary) ipsttp = 0 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 0 (Dimensionless thermal flux at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated,2: CDO ) NALINF = 0 (Fluid initialization iterations) IFLXMW = 0 (ALE mass flux computation 0: thanks to vertices 1: thanks to mesh velocity) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: time dependency: fixed mesh output: every 10 time steps and at calculation end -5: name: directory: monitoring format: time_plot options: time dependency: fixed mesh output: every 1 time steps -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at calculation end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at calculation end Reading file: mesh_input Finished reading: mesh_input Extended neighborhood structures definition Number of cells: 4000 ---------------------------------------------------------- Number of cells + halo cells: 4000 ---------------------------------------------------------- Number of interior faces: 7780 ---------------------------------------------------------- Number of boundary faces: 8440 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 1 : [ 2 ; 3 [ = 4 2 : [ 3 ; 4 ] = 3996 ---------------------------------------------------------- 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 number of halo-adjacent elements: 4000 Numbering for interior faces: type: default number of halo-adjacent elements: 7780 Numbering for boundary faces: type: default number of halo-adjacent elements: 8440 ---------------------------------------------------------- Matrix bandwidth for volume mesh : 200 Matrix profile/lines for volume mesh : 200 Mesh coordinates: minimum and maximum X : 0.0000000e+00 1.0000000e+00 Y : 0.0000000e+00 1.0000000e-01 Z : 0.0000000e+00 1.0000000e-02 Mesh Number of cells: 4000 Number of interior faces: 7780 Number of boundary faces: 8440 Number of vertices: 8442 Groups: "inlet" boundary faces: 20 "outlet" boundary faces: 20 "symmetry" boundary faces: 8000 "wall" boundary faces: 400 --- Information on the volumes Minimum control volume = 2.5000000e-07 Maximum control volume = 2.5000000e-07 Total volume for the domain = 1.0000000e-03 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 0 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Computing geometric quantities (0.00472 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 4000 Volume = 1.0000000e-03 Surface = -1 (not computed) Volume zone "all_cells" id = 1 Number of cells = 4000 Volume = 1.0000000e-03 Surface = -1 (not computed) --- Information on boundary zones Boundary zone "boundary_faces" id = 0 Number of faces = 8440 Surface = 2.2200000e-01 Perimeter = -1 (not computed) Boundary zone "BC_1" id = 1 Number of faces = 20 Surface = 1.0000000e-03 Perimeter = -1 (not computed) Boundary zone "BC_2" id = 2 Number of faces = 20 Surface = 1.0000000e-03 Perimeter = -1 (not computed) Boundary zone "BC_3" id = 3 Number of faces = 8000 Surface = 2.0000000e-01 Perimeter = -1 (not computed) Boundary zone "BC_4" id = 4 Number of faces = 400 Surface = 2.0000000e-02 Perimeter = -1 (not computed) Extended neighborhood reduced by non-orthogonality -------------------------------------------------- Size of complete cell-cell connectivity: 15124 Size of filtered cell-cell conectivity: 0 15124 connections removed, for a ratio of 0 % used ALMAX = 0.10000E+00 (Characteristic length ) ALMAX is the cubic root of the domain volume. ------------------------------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 --------------------------------- dt 0.1000E+00 0.1000E+00 --------------------------------- ------------------------------------------------------------- Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 20 Smooth wall 5 400 Rough wall 6 0 Symmetry 4 8000 Free outlet 3 20 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E+00 TIME STEP NUMBER 1 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1000E+04 0.1000E+04 molecular_viscos 0.1000E+03 0.1000E+03 ----------------------------------------- Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 0.000000000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.00000E+00 0.00000E+00 Friction velocity uk : 0.00000E+00 0.00000E+00 Dimensionless distance yplus : 0.00000E+00 0.00000E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.59629E+01 448 0.38728E-01 0.44448E+01 0.10000E+02 c Velocity[X] 0.44440E+01 c Velocity[Y] 0.77990E-03 c Velocity[Z] 0.61907E-34 c Pressure 0.54918E-01 15 0.55254E-08 0.29339E+00 0.10000E+02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.48335 0.73011 0.66644 0.66644 v Velocity[Y] -0.13069 0.13069 -5.6516e-11 -5.6516e-11 v Velocity[Z] -3.3922e-17 3.7052e-17 -4.6256e-21 -4.6256e-21 v ǁVelocityǁ 0.48338 0.73011 0.6665 0.6665 v Pressure 16.667 6515.1 3328.3 3328.3 v CourantNb 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 800 1600 1556 1556 INSTANT 0.200000000E+00 TIME STEP NUMBER 2 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43970E+01 0.51640E+01 Friction velocity uk : 0.43970E+01 0.51640E+01 Dimensionless distance yplus : 0.10993E+00 0.12910E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.60714E+01 619 0.32184E-01 0.50204E-02 0.33580E+00 c Velocity[X] 0.49834E-02 c Velocity[Y] 0.36936E-04 c Velocity[Z] 0.98691E-35 c Pressure 0.51029E-01 15 0.49999E-08 0.27802E+00 0.10000E+02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.46099 0.75385 0.66646 0.66646 v Velocity[Y] -0.14888 0.14888 -4.7194e-11 -4.7194e-11 v Velocity[Z] -3.6802e-17 3.3126e-17 -7.6398e-21 -7.6398e-21 v ǁVelocityǁ 0.46108 0.75385 0.66654 0.66654 v Pressure 15.398 6008.7 3073.6 3073.6 v CourantNb 9.8399 16.051 13.372 13.372 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 813.33 2016.1 1573.4 1573.4 INSTANT 0.300000000E+00 TIME STEP NUMBER 3 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42941E+01 0.49944E+01 Friction velocity uk : 0.42941E+01 0.49944E+01 Dimensionless distance yplus : 0.10735E+00 0.12486E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.60745E+01 616 0.32090E-01 0.41290E-02 0.30412E+00 c Velocity[X] 0.41177E-02 c Velocity[Y] 0.11281E-04 c Velocity[Z] 0.13819E-33 c Pressure 0.46830E-01 15 0.39463E-08 0.21544E+00 0.47995E+01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.4415 0.76351 0.6663 0.6663 v Velocity[Y] -0.14367 0.14367 -4.7996e-11 -4.7996e-11 v Velocity[Z] -3.9195e-17 4.2203e-17 -2.5547e-21 -2.5547e-21 v ǁVelocityǁ 0.44215 0.76351 0.66638 0.66638 v Pressure 29.605 11561 5910 5910 v CourantNb 9.2952 16.383 13.376 13.376 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 812.47 2016.4 1573.4 1573.4 INSTANT 0.400000000E+00 TIME STEP NUMBER 4 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42024E+01 0.48294E+01 Friction velocity uk : 0.42024E+01 0.48294E+01 Dimensionless distance yplus : 0.10506E+00 0.12073E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.60785E+01 613 0.29421E-01 0.35131E-02 0.27995E+00 c Velocity[X] 0.35049E-02 c Velocity[Y] 0.81446E-05 c Velocity[Z] 0.98809E-34 c Pressure 0.43638E-01 15 0.98678E-08 0.17302E+00 0.30697E+01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.41431 0.77307 0.66616 0.66616 v Velocity[Y] -0.13835 0.13835 1.1592e-10 1.1592e-10 v Velocity[Z] -6.4648e-17 7.7986e-17 -3.7238e-21 -3.7238e-21 v ǁVelocityǁ 0.41486 0.77307 0.66624 0.66624 v Pressure 42.712 16693 8527.5 8527.5 v CourantNb 9.0475 16.361 13.375 13.375 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 811.66 2016.4 1573.4 1573.4 INSTANT 0.500000000E+00 TIME STEP NUMBER 5 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666997E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40709E+01 0.46719E+01 Friction velocity uk : 0.40709E+01 0.46719E+01 Dimensionless distance yplus : 0.10177E+00 0.11680E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.60835E+01 610 0.27502E-01 0.29934E-02 0.25774E+00 c Velocity[X] 0.29869E-02 c Velocity[Y] 0.64663E-05 c Velocity[Z] 0.68260E-34 c Pressure 0.41003E-01 15 0.79550E-08 0.14299E+00 0.22076E+01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.39315 0.78285 0.66603 0.66603 v Velocity[Y] -0.13441 0.13441 9.7181e-11 9.7181e-11 v Velocity[Z] -8.9288e-17 1.0767e-16 -5.7103e-21 -5.7103e-21 v ǁVelocityǁ 0.39359 0.78285 0.66611 0.66611 v Pressure 54.805 21436 10943 10943 v CourantNb 8.8547 16.394 13.374 13.374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 810.91 2016.4 1573.4 1573.4 INSTANT 0.600000000E+00 TIME STEP NUMBER 6 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39656E+01 0.45217E+01 Friction velocity uk : 0.39656E+01 0.45217E+01 Dimensionless distance yplus : 0.99140E-01 0.11304E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.60890E+01 607 0.26069E-01 0.25520E-02 0.23728E+00 c Velocity[X] 0.25470E-02 c Velocity[Y] 0.50841E-05 c Velocity[Z] 0.45936E-34 c Pressure 0.38702E-01 15 0.66088E-08 0.12079E+00 0.16926E+01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.37588 0.79281 0.66591 0.66591 v Velocity[Y] -0.13311 0.13311 8.2865e-11 8.2865e-11 v Velocity[Z] -1.0943e-16 1.3193e-16 -8.5695e-21 -8.5695e-21 v ǁVelocityǁ 0.37623 0.79281 0.666 0.666 v Pressure 65.963 25820 13172 13172 v CourantNb 8.5987 16.432 13.374 13.374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 810.22 2016.4 1573.4 1573.4 INSTANT 0.700000000E+00 TIME STEP NUMBER 7 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38775E+01 0.43787E+01 Friction velocity uk : 0.38775E+01 0.43787E+01 Dimensionless distance yplus : 0.96938E-01 0.10947E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.60950E+01 604 0.25361E-01 0.21758E-02 0.21838E+00 c Velocity[X] 0.21718E-02 c Velocity[Y] 0.40684E-05 c Velocity[Z] 0.29644E-34 c Pressure 0.36657E-01 14 0.85966E-08 0.10386E+00 0.13510E+01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.36134 0.80289 0.66581 0.66581 v Velocity[Y] -0.13169 0.13169 1.6511e-10 1.6511e-10 v Velocity[Z] -1.256e-16 1.5136e-16 -9.7208e-21 -9.7208e-21 v ǁVelocityǁ 0.36164 0.80289 0.66589 0.66589 v Pressure 76.257 29873 15229 15229 v CourantNb 8.3618 16.476 13.374 13.374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 809.59 2016.5 1573.4 1573.4 INSTANT 0.800000000E+00 TIME STEP NUMBER 8 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38018E+01 0.42433E+01 Friction velocity uk : 0.38018E+01 0.42433E+01 Dimensionless distance yplus : 0.95045E-01 0.10608E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61011E+01 601 0.25364E-01 0.18557E-02 0.20100E+00 c Velocity[X] 0.18525E-02 c Velocity[Y] 0.32537E-05 c Velocity[Z] 0.17763E-34 c Pressure 0.34803E-01 14 0.73658E-08 0.90581E-01 0.11086E+01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.34871 0.81309 0.66571 0.66571 v Velocity[Y] -0.1302 0.1302 1.4212e-10 1.4212e-10 v Velocity[Z] -1.3825e-16 1.6653e-16 -1.0738e-20 -1.0738e-20 v ǁVelocityǁ 0.349 0.81309 0.6658 0.6658 v Pressure 85.755 33620 17127 17127 v CourantNb 8.1421 16.522 13.374 13.374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 809 2016.5 1573.4 1573.4 INSTANT 0.900000000E+00 TIME STEP NUMBER 9 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37348E+01 0.41156E+01 Friction velocity uk : 0.37348E+01 0.41156E+01 Dimensionless distance yplus : 0.93369E-01 0.10289E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61073E+01 598 0.25470E-01 0.15827E-02 0.18498E+00 c Velocity[X] 0.15801E-02 c Velocity[Y] 0.26320E-05 c Velocity[Z] 0.10494E-34 c Pressure 0.33109E-01 14 0.63761E-08 0.79925E-01 0.92821E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.33763 0.82335 0.66561 0.66561 v Velocity[Y] -0.12852 0.12852 1.2115e-10 1.2115e-10 v Velocity[Z] -1.4815e-16 1.78e-16 -1.1598e-20 -1.1598e-20 v ǁVelocityǁ 0.33792 0.82335 0.66571 0.66571 v Pressure 94.518 37084 18879 18879 v CourantNb 7.9074 16.569 13.375 13.375 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 808.46 2016.6 1573.4 1573.4 INSTANT 0.100000000E+01 TIME STEP NUMBER 10 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36750E+01 0.39991E+01 Friction velocity uk : 0.36750E+01 0.39991E+01 Dimensionless distance yplus : 0.91874E-01 0.99979E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61137E+01 595 0.25518E-01 0.13501E-02 0.17026E+00 c Velocity[X] 0.13480E-02 c Velocity[Y] 0.21520E-05 c Velocity[Z] 0.55519E-35 c Pressure 0.31552E-01 14 0.55834E-08 0.71216E-01 0.78905E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.32793 0.83557 0.66553 0.66553 v Velocity[Y] -0.12671 0.12671 1.0256e-10 1.0256e-10 v Velocity[Z] -1.5502e-16 1.8619e-16 -1.1947e-20 -1.1947e-20 v ǁVelocityǁ 0.32822 0.83557 0.66562 0.66562 v Pressure 102.6 40287 20496 20496 v CourantNb 7.6631 16.615 13.376 13.376 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 807.96 2016.6 1573.4 1573.4 INSTANT 0.110000000E+01 TIME STEP NUMBER 11 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36218E+01 0.39798E+01 Friction velocity uk : 0.36218E+01 0.39798E+01 Dimensionless distance yplus : 0.90544E-01 0.99496E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61199E+01 592 0.25574E-01 0.11519E-02 0.15673E+00 c Velocity[X] 0.11502E-02 c Velocity[Y] 0.17629E-05 c Velocity[Z] 0.24908E-35 c Pressure 0.30107E-01 14 0.49233E-08 0.63973E-01 0.67879E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.31931 0.84791 0.66544 0.66544 v Velocity[Y] -0.12479 0.12479 8.753e-11 8.753e-11 v Velocity[Z] -1.5959e-16 1.9158e-16 -1.1979e-20 -1.1979e-20 v ǁVelocityǁ 0.31961 0.84791 0.66554 0.66554 v Pressure 110.06 43249 21987 21987 v CourantNb 7.4104 16.733 13.377 13.377 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 807.49 2016.7 1573.4 1573.4 INSTANT 0.120000000E+01 TIME STEP NUMBER 12 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35738E+01 0.39629E+01 Friction velocity uk : 0.35738E+01 0.39629E+01 Dimensionless distance yplus : 0.89346E-01 0.99073E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61261E+01 589 0.25621E-01 0.98288E-03 0.14428E+00 c Velocity[X] 0.98143E-03 c Velocity[Y] 0.14502E-05 c Velocity[Z] 0.89632E-36 c Pressure 0.28764E-01 14 0.43649E-08 0.57872E-01 0.58952E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.3116 0.85929 0.66537 0.66537 v Velocity[Y] -0.12279 0.12279 7.3309e-11 7.3309e-11 v Velocity[Z] -1.6214e-16 1.949e-16 -1.2632e-20 -1.2632e-20 v ǁVelocityǁ 0.31191 0.85929 0.66547 0.66547 v Pressure 116.94 45988 23364 23364 v CourantNb 7.068 16.958 13.379 13.379 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 807.07 2016.7 1573.4 1573.4 INSTANT 0.130000000E+01 TIME STEP NUMBER 13 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35304E+01 0.39479E+01 Friction velocity uk : 0.35304E+01 0.39479E+01 Dimensionless distance yplus : 0.88260E-01 0.98698E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61321E+01 586 0.25658E-01 0.83866E-03 0.13284E+00 c Velocity[X] 0.83746E-03 c Velocity[Y] 0.11922E-05 c Velocity[Z] 0.23168E-36 c Pressure 0.27513E-01 14 0.40985E-08 0.52672E-01 0.51600E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.30397 0.86979 0.66529 0.66529 v Velocity[Y] -0.1208 0.1208 5.3694e-12 5.3694e-12 v Velocity[Z] -1.6269e-16 1.9545e-16 -1.2651e-20 -1.2651e-20 v ǁVelocityǁ 0.30416 0.86979 0.6654 0.6654 v Pressure 123.29 48520 24634 24634 v CourantNb 6.6751 17.186 13.382 13.382 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 806.68 2016.7 1573.4 1573.4 INSTANT 0.140000000E+01 TIME STEP NUMBER 14 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667005E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34870E+01 0.39345E+01 Friction velocity uk : 0.34870E+01 0.39345E+01 Dimensionless distance yplus : 0.87174E-01 0.98362E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61385E+01 583 0.25693E-01 0.71578E-03 0.12233E+00 c Velocity[X] 0.71480E-03 c Velocity[Y] 0.98160E-06 c Velocity[Z] 0.18966E-36 c Pressure 0.26342E-01 15 0.93194E-08 0.48193E-01 0.45457E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.2951 0.87948 0.66523 0.66523 v Velocity[Y] -0.11966 0.11966 7.4007e-10 7.4007e-10 v Velocity[Z] -1.6261e-16 1.9502e-16 -1.2426e-20 -1.2426e-20 v ǁVelocityǁ 0.29533 0.87948 0.66533 0.66533 v Pressure 129.15 50862 25807 25807 v CourantNb 6.3126 17.396 13.384 13.384 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 806.31 2016.8 1573.4 1573.4 INSTANT 0.150000000E+01 TIME STEP NUMBER 15 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34357E+01 0.39228E+01 Friction velocity uk : 0.34357E+01 0.39228E+01 Dimensionless distance yplus : 0.85893E-01 0.98071E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61442E+01 580 0.25704E-01 0.61096E-03 0.11268E+00 c Velocity[X] 0.61014E-03 c Velocity[Y] 0.82129E-06 c Velocity[Z] 0.57734E-36 c Pressure 0.25237E-01 14 0.97128E-08 0.44289E-01 0.40263E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.28348 0.88842 0.66516 0.66516 v Velocity[Y] -0.11836 0.11836 8.576e-10 8.576e-10 v Velocity[Z] -1.6034e-16 1.9259e-16 -1.2305e-20 -1.2305e-20 v ǁVelocityǁ 0.28348 0.88842 0.66527 0.66527 v Pressure 134.56 53028 26889 26889 v CourantNb 5.9781 17.59 13.387 13.387 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 805.98 2016.8 1573.4 1573.4 INSTANT 0.160000000E+01 TIME STEP NUMBER 16 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33674E+01 0.39122E+01 Friction velocity uk : 0.33674E+01 0.39122E+01 Dimensionless distance yplus : 0.84184E-01 0.97806E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61497E+01 577 0.25783E-01 0.52148E-03 0.10380E+00 c Velocity[X] 0.52079E-03 c Velocity[Y] 0.68062E-06 c Velocity[Z] 0.10138E-35 c Pressure 0.24198E-01 14 0.88143E-08 0.40869E-01 0.35827E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.26924 0.89667 0.6651 0.6651 v Velocity[Y] -0.11795 0.11795 7.9459e-10 7.9459e-10 v Velocity[Z] -1.5777e-16 1.89e-16 -1.2297e-20 -1.2297e-20 v ǁVelocityǁ 0.26924 0.89667 0.66521 0.66521 v Pressure 139.54 55032 27887 27887 v CourantNb 5.6695 17.768 13.389 13.389 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 805.67 2016.8 1573.4 1573.4 INSTANT 0.170000000E+01 TIME STEP NUMBER 17 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32817E+01 0.39024E+01 Friction velocity uk : 0.32817E+01 0.39024E+01 Dimensionless distance yplus : 0.82043E-01 0.97561E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61549E+01 574 0.25862E-01 0.44511E-03 0.95634E-01 c Velocity[X] 0.44452E-03 c Velocity[Y] 0.59121E-06 c Velocity[Z] 0.14888E-35 c Pressure 0.23221E-01 14 0.80343E-08 0.37855E-01 0.32006E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.25611 0.90428 0.66504 0.66504 v Velocity[Y] -0.11757 0.11757 7.4537e-10 7.4537e-10 v Velocity[Z] -1.5447e-16 1.8462e-16 -1.2337e-20 -1.2337e-20 v ǁVelocityǁ 0.25611 0.90428 0.66515 0.66515 v Pressure 144.14 56884 28808 28808 v CourantNb 5.3848 17.933 13.391 13.391 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 805.38 2016.8 1573.4 1573.4 INSTANT 0.180000000E+01 TIME STEP NUMBER 18 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32007E+01 0.38934E+01 Friction velocity uk : 0.32007E+01 0.38934E+01 Dimensionless distance yplus : 0.80017E-01 0.97334E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61599E+01 571 0.25943E-01 0.37994E-03 0.88125E-01 c Velocity[X] 0.37944E-03 c Velocity[Y] 0.50182E-06 c Velocity[Z] 0.20324E-35 c Pressure 0.22301E-01 14 0.73477E-08 0.35182E-01 0.28691E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.24399 0.91131 0.66499 0.66499 v Velocity[Y] -0.11709 0.11709 7.0186e-10 7.0186e-10 v Velocity[Z] -1.5029e-16 1.7989e-16 -1.1436e-20 -1.1436e-20 v ǁVelocityǁ 0.24399 0.91131 0.6651 0.6651 v Pressure 148.39 58598 29658 29658 v CourantNb 5.1221 18.086 13.393 13.393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 805.12 2016.9 1573.4 1573.4 INSTANT 0.190000000E+01 TIME STEP NUMBER 19 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31240E+01 0.38850E+01 Friction velocity uk : 0.31240E+01 0.38850E+01 Dimensionless distance yplus : 0.78101E-01 0.97124E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61646E+01 568 0.26019E-01 0.32436E-03 0.81224E-01 c Velocity[X] 0.32393E-03 c Velocity[Y] 0.43024E-06 c Velocity[Z] 0.25585E-35 c Pressure 0.21432E-01 13 0.98006E-08 0.32794E-01 0.25796E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.23281 0.91778 0.66494 0.66494 v Velocity[Y] -0.11651 0.11651 7.2204e-10 7.2204e-10 v Velocity[Z] -1.4562e-16 1.7414e-16 -1.1646e-20 -1.1646e-20 v ǁVelocityǁ 0.23281 0.91778 0.66505 0.66505 v Pressure 152.31 60184 30443 30443 v CourantNb 4.8798 18.226 13.395 13.395 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 804.88 2016.9 1573.4 1573.4 INSTANT 0.200000000E+01 TIME STEP NUMBER 20 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30516E+01 0.38772E+01 Friction velocity uk : 0.30516E+01 0.38772E+01 Dimensionless distance yplus : 0.76290E-01 0.96929E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61691E+01 565 0.26089E-01 0.27693E-03 0.74876E-01 c Velocity[X] 0.27656E-03 c Velocity[Y] 0.37139E-06 c Velocity[Z] 0.31293E-35 c Pressure 0.20608E-01 13 0.90135E-08 0.30649E-01 0.23253E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.22249 0.92376 0.66489 0.66489 v Velocity[Y] -0.11585 0.11585 6.8332e-10 6.8332e-10 v Velocity[Z] -1.403e-16 1.6761e-16 -1.1394e-20 -1.1394e-20 v ǁVelocityǁ 0.22249 0.92376 0.665 0.665 v Pressure 155.92 61651 31167 31167 v CourantNb 4.6561 18.356 13.396 13.396 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 804.66 2016.9 1573.4 1573.4 INSTANT 0.210000000E+01 TIME STEP NUMBER 21 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29832E+01 0.38699E+01 Friction velocity uk : 0.29832E+01 0.38699E+01 Dimensionless distance yplus : 0.74581E-01 0.96746E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61734E+01 562 0.26158E-01 0.23643E-03 0.69034E-01 c Velocity[X] 0.23611E-03 c Velocity[Y] 0.32248E-06 c Velocity[Z] 0.31662E-35 c Pressure 0.19828E-01 13 0.83153E-08 0.28716E-01 0.21009E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.21297 0.92928 0.66484 0.66484 v Velocity[Y] -0.11513 0.11513 6.517e-10 6.517e-10 v Velocity[Z] -1.3532e-16 1.6128e-16 -1.202e-20 -1.202e-20 v ǁVelocityǁ 0.21297 0.92928 0.66495 0.66495 v Pressure 159.25 63008 31835 31835 v CourantNb 4.4498 18.475 13.398 13.398 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 804.45 2016.9 1573.4 1573.4 INSTANT 0.220000000E+01 TIME STEP NUMBER 22 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29187E+01 0.38630E+01 Friction velocity uk : 0.29187E+01 0.38630E+01 Dimensionless distance yplus : 0.72967E-01 0.96576E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61774E+01 559 0.26018E-01 0.20192E-03 0.63665E-01 c Velocity[X] 0.20161E-03 c Velocity[Y] 0.31176E-06 c Velocity[Z] 0.78781E-35 c Pressure 0.19090E-01 13 0.76937E-08 0.26968E-01 0.19021E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.20419 0.93437 0.66479 0.66479 v Velocity[Y] -0.11433 0.11433 6.2107e-10 6.2107e-10 v Velocity[Z] -1.2673e-16 1.5109e-16 -1.2274e-20 -1.2274e-20 v ǁVelocityǁ 0.20419 0.93437 0.66491 0.66491 v Pressure 162.33 64263 32452 32452 v CourantNb 4.2594 18.586 13.399 13.399 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 804.26 2016.9 1573.4 1573.4 INSTANT 0.230000000E+01 TIME STEP NUMBER 23 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28579E+01 0.38566E+01 Friction velocity uk : 0.28579E+01 0.38566E+01 Dimensionless distance yplus : 0.71447E-01 0.96414E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61813E+01 556 0.25648E-01 0.17243E-03 0.58719E-01 c Velocity[X] 0.17209E-03 c Velocity[Y] 0.33241E-06 c Velocity[Z] 0.91449E-35 c Pressure 0.18389E-01 13 0.71162E-08 0.25379E-01 0.17251E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.19608 0.93907 0.66475 0.66475 v Velocity[Y] -0.11343 0.11343 5.9209e-10 5.9209e-10 v Velocity[Z] -1.1786e-16 1.4016e-16 -1.0181e-20 -1.0181e-20 v ǁVelocityǁ 0.19608 0.93907 0.66487 0.66487 v Pressure 165.17 65425 33020 33020 v CourantNb 4.0837 18.687 13.4 13.4 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 804.08 2016.9 1573.4 1573.4 INSTANT 0.240000000E+01 TIME STEP NUMBER 24 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28006E+01 0.38505E+01 Friction velocity uk : 0.28006E+01 0.38505E+01 Dimensionless distance yplus : 0.70015E-01 0.96263E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61849E+01 553 0.25295E-01 0.14722E-03 0.54160E-01 c Velocity[X] 0.14692E-03 c Velocity[Y] 0.29933E-06 c Velocity[Z] 0.77949E-35 c Pressure 0.17720E-01 13 0.66074E-08 0.23925E-01 0.15671E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.1886 0.9434 0.66471 0.66471 v Velocity[Y] -0.11258 0.11258 5.6389e-10 5.6389e-10 v Velocity[Z] -1.0945e-16 1.3017e-16 -1.1626e-20 -1.1626e-20 v ǁVelocityǁ 0.1886 0.9434 0.66483 0.66483 v Pressure 167.79 66500 33545 33545 v CourantNb 3.9216 18.781 13.401 13.401 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803.92 2016.9 1573.4 1573.4 INSTANT 0.250000000E+01 TIME STEP NUMBER 25 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27467E+01 0.38450E+01 Friction velocity uk : 0.27467E+01 0.38450E+01 Dimensionless distance yplus : 0.68666E-01 0.96124E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61883E+01 550 0.24986E-01 0.12567E-03 0.49956E-01 c Velocity[X] 0.12541E-03 c Velocity[Y] 0.26054E-06 c Velocity[Z] 0.67124E-35 c Pressure 0.17079E-01 13 0.61698E-08 0.22589E-01 0.14257E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.1817 0.9474 0.66467 0.66467 v Velocity[Y] -0.11173 0.11173 5.4168e-10 5.4168e-10 v Velocity[Z] -1.0165e-16 1.2072e-16 -1.0992e-20 -1.0992e-20 v ǁVelocityǁ 0.1817 0.9474 0.66479 0.66479 v Pressure 170.2 67495 34030 34030 v CourantNb 3.772 18.868 13.403 13.403 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803.77 2017 1573.4 1573.4 INSTANT 0.260000000E+01 TIME STEP NUMBER 26 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26959E+01 0.38398E+01 Friction velocity uk : 0.26959E+01 0.38398E+01 Dimensionless distance yplus : 0.67398E-01 0.95995E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61915E+01 548 0.24552E-01 0.10731E-03 0.46090E-01 c Velocity[X] 0.10707E-03 c Velocity[Y] 0.24546E-06 c Velocity[Z] 0.56948E-35 c Pressure 0.16472E-01 13 0.57752E-08 0.21366E-01 0.12987E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.17533 0.9511 0.66464 0.66464 v Velocity[Y] -0.11081 0.11081 5.1984e-10 5.1984e-10 v Velocity[Z] -9.4566e-17 1.1216e-16 -1.1427e-20 -1.1427e-20 v ǁVelocityǁ 0.17533 0.9511 0.66475 0.66475 v Pressure 172.43 68416 34477 34477 v CourantNb 3.6339 18.948 13.404 13.404 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803.63 2017 1573.4 1573.4 INSTANT 0.270000000E+01 TIME STEP NUMBER 27 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26482E+01 0.38348E+01 Friction velocity uk : 0.26482E+01 0.38348E+01 Dimensionless distance yplus : 0.66206E-01 0.95870E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61945E+01 545 0.24110E-01 0.91633E-04 0.42528E-01 c Velocity[X] 0.91405E-04 c Velocity[Y] 0.22840E-06 c Velocity[Z] 0.48611E-35 c Pressure 0.15894E-01 13 0.53998E-08 0.20241E-01 0.11844E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.16945 0.95451 0.6646 0.6646 v Velocity[Y] -0.1098 0.1098 5.0075e-10 5.0075e-10 v Velocity[Z] -8.8032e-17 1.0425e-16 -1.3202e-20 -1.3202e-20 v ǁVelocityǁ 0.16945 0.95451 0.66472 0.66472 v Pressure 174.49 69269 34890 34890 v CourantNb 3.5064 19.022 13.404 13.404 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803.51 2017 1573.4 1573.4 INSTANT 0.280000000E+01 TIME STEP NUMBER 28 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26034E+01 0.38300E+01 Friction velocity uk : 0.26034E+01 0.38300E+01 Dimensionless distance yplus : 0.65086E-01 0.95751E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61973E+01 542 0.23605E-01 0.78158E-04 0.39223E-01 c Velocity[X] 0.77984E-04 c Velocity[Y] 0.17380E-06 c Velocity[Z] 0.41183E-35 c Pressure 0.15357E-01 13 0.50384E-08 0.19219E-01 0.10813E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.16402 0.95766 0.66457 0.66457 v Velocity[Y] -0.10874 0.10874 4.8012e-10 4.8012e-10 v Velocity[Z] -8.2085e-17 9.6937e-17 -1.3784e-20 -1.3784e-20 v ǁVelocityǁ 0.16402 0.95766 0.66469 0.66469 v Pressure 176.38 70058 35270 35270 v CourantNb 3.3887 19.09 13.405 13.405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803.39 2017 1573.4 1573.4 INSTANT 0.290000000E+01 TIME STEP NUMBER 29 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25614E+01 0.38253E+01 Friction velocity uk : 0.25614E+01 0.38253E+01 Dimensionless distance yplus : 0.64035E-01 0.95633E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.61999E+01 539 0.23012E-01 0.66664E-04 0.36178E-01 c Velocity[X] 0.66518E-04 c Velocity[Y] 0.14547E-06 c Velocity[Z] 0.35162E-35 c Pressure 0.14858E-01 12 0.97170E-08 0.18291E-01 0.98805E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.159 0.96057 0.66454 0.66454 v Velocity[Y] -0.10759 0.10759 5.0782e-10 5.0782e-10 v Velocity[Z] -7.6559e-17 9.0201e-17 -1.344e-20 -1.344e-20 v ǁVelocityǁ 0.159 0.96057 0.66465 0.66465 v Pressure 178.13 70789 35622 35622 v CourantNb 3.2801 19.153 13.406 13.406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803.28 2017 1573.4 1573.4 INSTANT 0.300000000E+01 TIME STEP NUMBER 30 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25219E+01 0.38207E+01 Friction velocity uk : 0.25219E+01 0.38207E+01 Dimensionless distance yplus : 0.63048E-01 0.95518E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62023E+01 536 0.22415E-01 0.56943E-04 0.33397E-01 c Velocity[X] 0.56804E-04 c Velocity[Y] 0.13919E-06 c Velocity[Z] 0.30352E-35 c Pressure 0.14385E-01 12 0.90617E-08 0.17434E-01 0.90366E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.15437 0.96325 0.66451 0.66451 v Velocity[Y] -0.10642 0.10642 4.8449e-10 4.8449e-10 v Velocity[Z] -7.1303e-17 8.3984e-17 -1.2419e-20 -1.2419e-20 v ǁVelocityǁ 0.15437 0.96325 0.66462 0.66462 v Pressure 179.75 71466 35946 35946 v CourantNb 3.1797 19.211 13.407 13.407 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803.18 2017 1573.4 1573.4 INSTANT 0.310000000E+01 TIME STEP NUMBER 31 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24849E+01 0.38164E+01 Friction velocity uk : 0.24849E+01 0.38164E+01 Dimensionless distance yplus : 0.62124E-01 0.95411E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62046E+01 533 0.21821E-01 0.48667E-04 0.30841E-01 c Velocity[X] 0.48530E-04 c Velocity[Y] 0.13624E-06 c Velocity[Z] 0.25439E-35 c Pressure 0.13936E-01 12 0.84791E-08 0.16640E-01 0.82711E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.1501 0.96574 0.66448 0.66448 v Velocity[Y] -0.10561 0.10561 4.6075e-10 4.6075e-10 v Velocity[Z] -6.6626e-17 7.8243e-17 -1.3726e-20 -1.3726e-20 v ǁVelocityǁ 0.1501 0.96574 0.66459 0.66459 v Pressure 181.24 72093 36245 36245 v CourantNb 3.087 19.265 13.408 13.408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803.09 2017 1573.4 1573.4 INSTANT 0.320000000E+01 TIME STEP NUMBER 32 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24503E+01 0.38124E+01 Friction velocity uk : 0.24503E+01 0.38124E+01 Dimensionless distance yplus : 0.61257E-01 0.95309E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62072E+01 530 0.21232E-01 0.41608E-04 0.28488E-01 c Velocity[X] 0.41478E-04 c Velocity[Y] 0.12972E-06 c Velocity[Z] 0.21568E-35 c Pressure 0.13509E-01 12 0.79220E-08 0.15903E-01 0.75758E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.14615 0.96803 0.66445 0.66445 v Velocity[Y] -0.10484 0.10484 4.3887e-10 4.3887e-10 v Velocity[Z] -6.225e-17 7.2951e-17 -1.3101e-20 -1.3101e-20 v ǁVelocityǁ 0.14615 0.96803 0.66457 0.66457 v Pressure 182.61 72674 36521 36521 v CourantNb 3.0014 19.314 13.408 13.408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 803 2017 1573.4 1573.4 INSTANT 0.330000000E+01 TIME STEP NUMBER 33 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24178E+01 0.38087E+01 Friction velocity uk : 0.24178E+01 0.38087E+01 Dimensionless distance yplus : 0.60446E-01 0.95217E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62098E+01 527 0.20645E-01 0.35586E-04 0.26321E-01 c Velocity[X] 0.35457E-04 c Velocity[Y] 0.12881E-06 c Velocity[Z] 0.18356E-35 c Pressure 0.13101E-01 14 0.84182E-08 0.15216E-01 0.69434E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.1425 0.97015 0.66443 0.66443 v Velocity[Y] -0.104 0.104 1.3596e-09 1.3596e-09 v Velocity[Z] -5.8248e-17 6.8126e-17 -1.3014e-20 -1.3014e-20 v ǁVelocityǁ 0.1425 0.97015 0.66454 0.66454 v Pressure 183.88 73212 36776 36776 v CourantNb 2.9222 19.36 13.409 13.409 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.93 2017.1 1573.4 1573.4 INSTANT 0.340000000E+01 TIME STEP NUMBER 34 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666997E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23875E+01 0.38063E+01 Friction velocity uk : 0.23875E+01 0.38063E+01 Dimensionless distance yplus : 0.59687E-01 0.95157E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62116E+01 524 0.20090E-01 0.30455E-04 0.24328E-01 c Velocity[X] 0.30328E-04 c Velocity[Y] 0.12633E-06 c Velocity[Z] 0.15981E-35 c Pressure 0.12705E-01 13 0.98819E-08 0.14567E-01 0.63675E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.13913 0.97212 0.6644 0.6644 v Velocity[Y] -0.10316 0.10316 1.5101e-09 1.5101e-09 v Velocity[Z] -5.4515e-17 6.3574e-17 -1.1416e-20 -1.1416e-20 v ǁVelocityǁ 0.13913 0.97212 0.66451 0.66451 v Pressure 185.05 73711 37011 37011 v CourantNb 2.8491 19.402 13.409 13.409 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.85 2017.1 1573.4 1573.4 INSTANT 0.350000000E+01 TIME STEP NUMBER 35 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666997E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23590E+01 0.38031E+01 Friction velocity uk : 0.23590E+01 0.38031E+01 Dimensionless distance yplus : 0.58976E-01 0.95077E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62134E+01 521 0.19530E-01 0.26058E-04 0.22485E-01 c Velocity[X] 0.25932E-04 c Velocity[Y] 0.12608E-06 c Velocity[Z] 0.13591E-35 c Pressure 0.12325E-01 13 0.92719E-08 0.13959E-01 0.58425E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.13601 0.97393 0.66438 0.66438 v Velocity[Y] -0.10229 0.10229 1.3835e-09 1.3835e-09 v Velocity[Z] -5.1025e-17 5.9432e-17 -1.2221e-20 -1.2221e-20 v ǁVelocityǁ 0.13601 0.97393 0.66449 0.66449 v Pressure 186.13 74173 37228 37228 v CourantNb 2.7814 19.442 13.41 13.41 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.79 2017.1 1573.4 1573.4 INSTANT 0.360000000E+01 TIME STEP NUMBER 36 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666997E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23325E+01 0.37999E+01 Friction velocity uk : 0.23325E+01 0.37999E+01 Dimensionless distance yplus : 0.58312E-01 0.94998E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62150E+01 518 0.18978E-01 0.22308E-04 0.20789E-01 c Velocity[X] 0.22183E-04 c Velocity[Y] 0.12468E-06 c Velocity[Z] 0.11426E-35 c Pressure 0.11960E-01 13 0.87077E-08 0.13387E-01 0.53633E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.13313 0.97562 0.66436 0.66436 v Velocity[Y] -0.10141 0.10141 1.264e-09 1.264e-09 v Velocity[Z] -4.7899e-17 5.5599e-17 -1.1266e-20 -1.1266e-20 v ǁVelocityǁ 0.13313 0.97562 0.66446 0.66446 v Pressure 187.13 74601 37428 37428 v CourantNb 2.7188 19.478 13.41 13.41 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.73 2017.1 1573.4 1573.4 INSTANT 0.370000000E+01 TIME STEP NUMBER 37 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23076E+01 0.37970E+01 Friction velocity uk : 0.23076E+01 0.37970E+01 Dimensionless distance yplus : 0.57691E-01 0.94924E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62165E+01 515 0.18438E-01 0.19102E-04 0.19224E-01 c Velocity[X] 0.18979E-04 c Velocity[Y] 0.12346E-06 c Velocity[Z] 0.97314E-36 c Pressure 0.11608E-01 13 0.81857E-08 0.12848E-01 0.49256E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.13047 0.97717 0.66434 0.66434 v Velocity[Y] -0.10052 0.10052 1.1507e-09 1.1507e-09 v Velocity[Z] -4.4971e-17 5.2104e-17 -1.2394e-20 -1.2394e-20 v ǁVelocityǁ 0.13047 0.97717 0.66444 0.66444 v Pressure 188.05 74998 37613 37613 v CourantNb 2.661 19.511 13.411 13.411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.67 2017.1 1573.4 1573.4 INSTANT 0.380000000E+01 TIME STEP NUMBER 38 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22844E+01 0.37942E+01 Friction velocity uk : 0.22844E+01 0.37942E+01 Dimensionless distance yplus : 0.57111E-01 0.94855E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62179E+01 512 0.17907E-01 0.16360E-04 0.17779E-01 c Velocity[X] 0.16238E-04 c Velocity[Y] 0.12232E-06 c Velocity[Z] 0.83318E-36 c Pressure 0.11269E-01 13 0.77028E-08 0.12340E-01 0.45255E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.128 0.97862 0.66431 0.66431 v Velocity[Y] -0.099615 0.099615 1.0435e-09 1.0435e-09 v Velocity[Z] -4.2249e-17 4.8906e-17 -9.7912e-21 -9.7912e-21 v ǁVelocityǁ 0.128 0.97862 0.66442 0.66442 v Pressure 188.89 75367 37784 37784 v CourantNb 2.6074 19.542 13.411 13.411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.62 2017.1 1573.4 1573.4 INSTANT 0.390000000E+01 TIME STEP NUMBER 39 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22628E+01 0.37916E+01 Friction velocity uk : 0.22628E+01 0.37916E+01 Dimensionless distance yplus : 0.56570E-01 0.94789E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62192E+01 509 0.17387E-01 0.14030E-04 0.16455E-01 c Velocity[X] 0.13911E-04 c Velocity[Y] 0.11896E-06 c Velocity[Z] 0.71363E-36 c Pressure 0.10942E-01 13 0.72547E-08 0.11859E-01 0.41595E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.12573 0.97995 0.66429 0.66429 v Velocity[Y] -0.098711 0.098711 9.4247e-10 9.4247e-10 v Velocity[Z] -3.976e-17 4.5912e-17 -1.0926e-20 -1.0926e-20 v ǁVelocityǁ 0.12573 0.97995 0.6644 0.6644 v Pressure 189.68 75708 37941 37941 v CourantNb 2.5579 19.571 13.411 13.411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.57 2017.1 1573.4 1573.4 INSTANT 0.400000000E+01 TIME STEP NUMBER 40 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22426E+01 0.37891E+01 Friction velocity uk : 0.22426E+01 0.37891E+01 Dimensionless distance yplus : 0.56064E-01 0.94727E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62204E+01 506 0.16881E-01 0.12030E-04 0.15228E-01 c Velocity[X] 0.11912E-04 c Velocity[Y] 0.11749E-06 c Velocity[Z] 0.60976E-36 c Pressure 0.10626E-01 13 0.68525E-08 0.11403E-01 0.38243E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.12362 0.9812 0.66428 0.66428 v Velocity[Y] -0.097801 0.097801 8.4202e-10 8.4202e-10 v Velocity[Z] -3.7478e-17 4.3098e-17 -9.3973e-21 -9.3973e-21 v ǁVelocityǁ 0.12362 0.9812 0.66438 0.66438 v Pressure 190.4 76025 38086 38086 v CourantNb 2.512 19.597 13.412 13.412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.52 2017.1 1573.4 1573.4 INSTANT 0.410000000E+01 TIME STEP NUMBER 41 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22237E+01 0.37867E+01 Friction velocity uk : 0.22237E+01 0.37867E+01 Dimensionless distance yplus : 0.55593E-01 0.94668E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62213E+01 503 0.16380E-01 0.10335E-04 0.14107E-01 c Velocity[X] 0.10224E-04 c Velocity[Y] 0.11079E-06 c Velocity[Z] 0.52046E-36 c Pressure 0.10318E-01 12 0.99345E-08 0.10969E-01 0.35172E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.12167 0.98235 0.66426 0.66426 v Velocity[Y] -0.096913 0.096913 9.4009e-10 9.4009e-10 v Velocity[Z] -3.5353e-17 4.0571e-17 -9.2984e-21 -9.2984e-21 v ǁVelocityǁ 0.12167 0.98235 0.66436 0.66436 v Pressure 191.06 76319 38220 38220 v CourantNb 2.4694 19.622 13.412 13.412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.48 2017.1 1573.4 1573.4 INSTANT 0.420000000E+01 TIME STEP NUMBER 42 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22061E+01 0.37845E+01 Friction velocity uk : 0.22061E+01 0.37845E+01 Dimensionless distance yplus : 0.55153E-01 0.94613E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62224E+01 500 0.15885E-01 0.88641E-05 0.13059E-01 c Velocity[X] 0.87532E-05 c Velocity[Y] 0.11090E-06 c Velocity[Z] 0.45141E-36 c Pressure 0.10019E-01 12 0.94473E-08 0.10555E-01 0.32358E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.11987 0.98342 0.66424 0.66424 v Velocity[Y] -0.09604 0.09604 8.4702e-10 8.4702e-10 v Velocity[Z] -3.337e-17 3.8208e-17 -9.2712e-21 -9.2712e-21 v ǁVelocityǁ 0.11987 0.98342 0.66434 0.66434 v Pressure 191.68 76591 38344 38344 v CourantNb 2.4302 19.644 13.412 13.412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.44 2017.1 1573.4 1573.4 INSTANT 0.430000000E+01 TIME STEP NUMBER 43 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21897E+01 0.37825E+01 Friction velocity uk : 0.21897E+01 0.37825E+01 Dimensionless distance yplus : 0.54743E-01 0.94562E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62234E+01 497 0.15404E-01 0.76108E-05 0.12095E-01 c Velocity[X] 0.75016E-05 c Velocity[Y] 0.10915E-06 c Velocity[Z] 0.38065E-36 c Pressure 0.97296E-02 12 0.90104E-08 0.10161E-01 0.29776E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.11821 0.98442 0.66422 0.66422 v Velocity[Y] -0.095162 0.095162 7.864e-10 7.864e-10 v Velocity[Z] -3.1587e-17 3.604e-17 -8.1625e-21 -8.1625e-21 v ǁVelocityǁ 0.11821 0.98442 0.66432 0.66432 v Pressure 192.25 76844 38458 38458 v CourantNb 2.3937 19.665 13.413 13.413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.41 2017.2 1573.4 1573.4 INSTANT 0.440000000E+01 TIME STEP NUMBER 44 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21744E+01 0.37805E+01 Friction velocity uk : 0.21744E+01 0.37805E+01 Dimensionless distance yplus : 0.54361E-01 0.94513E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62243E+01 494 0.14937E-01 0.65403E-05 0.11208E-01 c Velocity[X] 0.64334E-05 c Velocity[Y] 0.10687E-06 c Velocity[Z] 0.32328E-36 c Pressure 0.94497E-02 12 0.85778E-08 0.97868E-02 0.27407E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.11666 0.98534 0.66421 0.66421 v Velocity[Y] -0.094289 0.094289 6.748e-10 6.748e-10 v Velocity[Z] -2.99e-17 3.4056e-17 -7.6162e-21 -7.6162e-21 v ǁVelocityǁ 0.11666 0.98534 0.66431 0.66431 v Pressure 192.77 77079 38564 38564 v CourantNb 2.3598 19.685 13.413 13.413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.38 2017.2 1573.4 1573.4 INSTANT 0.450000000E+01 TIME STEP NUMBER 45 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21602E+01 0.37786E+01 Friction velocity uk : 0.21602E+01 0.37786E+01 Dimensionless distance yplus : 0.54005E-01 0.94466E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62252E+01 491 0.14483E-01 0.56237E-05 0.10389E-01 c Velocity[X] 0.55192E-05 c Velocity[Y] 0.10456E-06 c Velocity[Z] 0.27645E-36 c Pressure 0.91789E-02 12 0.81698E-08 0.94302E-02 0.25233E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.11524 0.98621 0.66419 0.66419 v Velocity[Y] -0.093419 0.093419 5.7503e-10 5.7503e-10 v Velocity[Z] -2.8382e-17 3.2239e-17 -7.5384e-21 -7.5384e-21 v ǁVelocityǁ 0.11524 0.98621 0.66429 0.66429 v Pressure 193.25 77297 38661 38661 v CourantNb 2.3287 19.703 13.413 13.413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.35 2017.2 1573.4 1573.4 INSTANT 0.460000000E+01 TIME STEP NUMBER 46 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21470E+01 0.37768E+01 Friction velocity uk : 0.21470E+01 0.37768E+01 Dimensionless distance yplus : 0.53674E-01 0.94421E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62260E+01 488 0.14042E-01 0.48391E-05 0.96334E-02 c Velocity[X] 0.47370E-05 c Velocity[Y] 0.10214E-06 c Velocity[Z] 0.23988E-36 c Pressure 0.89166E-02 12 0.78144E-08 0.90903E-02 0.23235E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.11392 0.98702 0.66418 0.66418 v Velocity[Y] -0.092555 0.092555 4.7722e-10 4.7722e-10 v Velocity[Z] -2.6963e-17 3.0535e-17 -8.1596e-21 -8.1596e-21 v ǁVelocityǁ 0.11392 0.98702 0.66427 0.66427 v Pressure 193.7 77500 38750 38750 v CourantNb 2.2994 19.72 13.413 13.413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.32 2017.2 1573.4 1573.4 INSTANT 0.470000000E+01 TIME STEP NUMBER 47 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666996E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21346E+01 0.37751E+01 Friction velocity uk : 0.21346E+01 0.37751E+01 Dimensionless distance yplus : 0.53366E-01 0.94378E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62267E+01 485 0.13613E-01 0.41671E-05 0.89367E-02 c Velocity[X] 0.40675E-05 c Velocity[Y] 0.99639E-07 c Velocity[Z] 0.20382E-36 c Pressure 0.86625E-02 12 0.74540E-08 0.87660E-02 0.21400E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.1127 0.98777 0.66416 0.66416 v Velocity[Y] -0.091696 0.091696 4.3746e-10 4.3746e-10 v Velocity[Z] -2.5637e-17 2.8963e-17 -6.9921e-21 -6.9921e-21 v ǁVelocityǁ 0.1127 0.98777 0.66426 0.66426 v Pressure 194.11 77688 38833 38833 v CourantNb 2.2727 19.735 13.414 13.414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.29 2017.2 1573.4 1573.4 INSTANT 0.480000000E+01 TIME STEP NUMBER 48 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21232E+01 0.37735E+01 Friction velocity uk : 0.21232E+01 0.37735E+01 Dimensionless distance yplus : 0.53079E-01 0.94337E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62274E+01 482 0.13197E-01 0.35914E-05 0.82939E-02 c Velocity[X] 0.34943E-05 c Velocity[Y] 0.97064E-07 c Velocity[Z] 0.17689E-36 c Pressure 0.84164E-02 12 0.71092E-08 0.84563E-02 0.19713E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.11156 0.98848 0.66415 0.66415 v Velocity[Y] -0.090844 0.090844 3.7669e-10 3.7669e-10 v Velocity[Z] -2.4421e-17 2.7491e-17 -7.8756e-21 -7.8756e-21 v ǁVelocityǁ 0.11156 0.98848 0.66424 0.66424 v Pressure 194.49 77862 38910 38910 v CourantNb 2.2475 19.749 13.414 13.414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.27 2017.2 1573.4 1573.4 INSTANT 0.490000000E+01 TIME STEP NUMBER 49 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21125E+01 0.37719E+01 Friction velocity uk : 0.21125E+01 0.37719E+01 Dimensionless distance yplus : 0.52812E-01 0.94298E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62281E+01 479 0.12800E-01 0.31007E-05 0.77044E-02 c Velocity[X] 0.30068E-05 c Velocity[Y] 0.93977E-07 c Velocity[Z] 0.15490E-36 c Pressure 0.81767E-02 12 0.67806E-08 0.81592E-02 0.18162E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.11052 0.98915 0.66414 0.66414 v Velocity[Y] -0.090031 0.090031 3.2107e-10 3.2107e-10 v Velocity[Z] -2.3325e-17 2.6154e-17 -6.5583e-21 -6.5583e-21 v ǁVelocityǁ 0.11052 0.98915 0.66423 0.66423 v Pressure 194.84 78025 38980 38980 v CourantNb 2.2245 19.763 13.414 13.414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.25 2017.2 1573.4 1573.4 INSTANT 0.500000000E+01 TIME STEP NUMBER 50 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21026E+01 0.37704E+01 Friction velocity uk : 0.21026E+01 0.37704E+01 Dimensionless distance yplus : 0.52564E-01 0.94261E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62287E+01 476 0.12422E-01 0.26772E-05 0.71572E-02 c Velocity[X] 0.25867E-05 c Velocity[Y] 0.90518E-07 c Velocity[Z] 0.13163E-36 c Pressure 0.79439E-02 12 0.64678E-08 0.78746E-02 0.16736E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10955 0.98978 0.66413 0.66413 v Velocity[Y] -0.089207 0.089207 2.7053e-10 2.7053e-10 v Velocity[Z] -2.2303e-17 2.4921e-17 -7.39e-21 -7.39e-21 v ǁVelocityǁ 0.10955 0.98978 0.66422 0.66422 v Pressure 195.16 78176 39045 39045 v CourantNb 2.2027 19.775 13.414 13.414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.23 2017.2 1573.4 1573.4 INSTANT 0.510000000E+01 TIME STEP NUMBER 51 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20933E+01 0.37690E+01 Friction velocity uk : 0.20933E+01 0.37690E+01 Dimensionless distance yplus : 0.52333E-01 0.94226E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62293E+01 473 0.12057E-01 0.23125E-05 0.66502E-02 c Velocity[X] 0.22244E-05 c Velocity[Y] 0.88120E-07 c Velocity[Z] 0.11621E-36 c Pressure 0.77187E-02 12 0.61737E-08 0.76028E-02 0.15424E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10865 0.99037 0.66411 0.66411 v Velocity[Y] -0.088383 0.088383 2.2476e-10 2.2476e-10 v Velocity[Z] -2.1356e-17 2.3784e-17 -6.2143e-21 -6.2143e-21 v ǁVelocityǁ 0.10865 0.99037 0.6642 0.6642 v Pressure 195.46 78316 39105 39105 v CourantNb 2.1829 19.786 13.414 13.414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.21 2017.2 1573.4 1573.4 INSTANT 0.520000000E+01 TIME STEP NUMBER 52 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20847E+01 0.37677E+01 Friction velocity uk : 0.20847E+01 0.37677E+01 Dimensionless distance yplus : 0.52119E-01 0.94192E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62298E+01 470 0.11704E-01 0.20009E-05 0.61846E-02 c Velocity[X] 0.19155E-05 c Velocity[Y] 0.85347E-07 c Velocity[Z] 0.94401E-37 c Pressure 0.75004E-02 12 0.58891E-08 0.73425E-02 0.14217E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10783 0.99093 0.6641 0.6641 v Velocity[Y] -0.087569 0.087569 1.8329e-10 1.8329e-10 v Velocity[Z] -2.0482e-17 2.2723e-17 -4.9973e-21 -4.9973e-21 v ǁVelocityǁ 0.10783 0.99093 0.66419 0.66419 v Pressure 195.73 78446 39161 39161 v CourantNb 2.1642 19.797 13.414 13.414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.19 2017.2 1573.4 1573.4 INSTANT 0.530000000E+01 TIME STEP NUMBER 53 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20768E+01 0.37664E+01 Friction velocity uk : 0.20768E+01 0.37664E+01 Dimensionless distance yplus : 0.51920E-01 0.94159E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62303E+01 467 0.11362E-01 0.17333E-05 0.57551E-02 c Velocity[X] 0.16507E-05 c Velocity[Y] 0.82574E-07 c Velocity[Z] 0.83010E-37 c Pressure 0.72886E-02 12 0.56167E-08 0.70931E-02 0.13106E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10706 0.99146 0.66409 0.66409 v Velocity[Y] -0.086764 0.086764 1.4637e-10 1.4637e-10 v Velocity[Z] -1.9674e-17 2.1765e-17 -5.2891e-21 -5.2891e-21 v ǁVelocityǁ 0.10706 0.99146 0.66418 0.66418 v Pressure 195.98 78568 39212 39212 v CourantNb 2.147 19.807 13.414 13.414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.18 2017.2 1573.4 1573.4 INSTANT 0.540000000E+01 TIME STEP NUMBER 54 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20694E+01 0.37651E+01 Friction velocity uk : 0.20694E+01 0.37651E+01 Dimensionless distance yplus : 0.51735E-01 0.94127E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62308E+01 464 0.11032E-01 0.15034E-05 0.53588E-02 c Velocity[X] 0.14236E-05 c Velocity[Y] 0.79816E-07 c Velocity[Z] 0.69955E-37 c Pressure 0.70832E-02 12 0.54774E-08 0.68540E-02 0.12083E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10635 0.99196 0.66408 0.66408 v Velocity[Y] -0.085968 0.085968 -9.6274e-12 -9.6274e-12 v Velocity[Z] -1.893e-17 2.0871e-17 -4.7084e-21 -4.7084e-21 v ǁVelocityǁ 0.10635 0.99196 0.66417 0.66417 v Pressure 196.22 78681 39259 39259 v CourantNb 2.1309 19.816 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.16 2017.2 1573.4 1573.4 INSTANT 0.550000000E+01 TIME STEP NUMBER 55 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667008E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20625E+01 0.37639E+01 Friction velocity uk : 0.20625E+01 0.37639E+01 Dimensionless distance yplus : 0.51563E-01 0.94097E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62312E+01 461 0.10710E-01 0.13066E-05 0.49949E-02 c Velocity[X] 0.12294E-05 c Velocity[Y] 0.77203E-07 c Velocity[Z] 0.67057E-37 c Pressure 0.68836E-02 12 0.52225E-08 0.66243E-02 0.11141E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.1057 0.99244 0.66407 0.66407 v Velocity[Y] -0.085189 0.085189 -3.2211e-11 -3.2211e-11 v Velocity[Z] -1.8226e-17 2.004e-17 -5.4866e-21 -5.4866e-21 v ǁVelocityǁ 0.1057 0.99244 0.66416 0.66416 v Pressure 196.43 78786 39303 39303 v CourantNb 2.1158 19.824 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.15 2017.2 1573.4 1573.4 INSTANT 0.560000000E+01 TIME STEP NUMBER 56 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667007E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20562E+01 0.37627E+01 Friction velocity uk : 0.20562E+01 0.37627E+01 Dimensionless distance yplus : 0.51404E-01 0.94068E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62316E+01 459 0.10398E-01 0.11377E-05 0.46602E-02 c Velocity[X] 0.10632E-05 c Velocity[Y] 0.74488E-07 c Velocity[Z] 0.59621E-37 c Pressure 0.66894E-02 12 0.49938E-08 0.64033E-02 0.10273E-01 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10509 0.99288 0.66406 0.66406 v Velocity[Y] -0.084429 0.084429 7.1144e-11 7.1144e-11 v Velocity[Z] -1.7606e-17 1.9292e-17 -3.4006e-21 -3.4006e-21 v ǁVelocityǁ 0.10509 0.99288 0.66414 0.66414 v Pressure 196.63 78884 39343 39343 v CourantNb 2.1021 19.832 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.14 2017.2 1573.4 1573.4 INSTANT 0.570000000E+01 TIME STEP NUMBER 57 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667005E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20502E+01 0.37616E+01 Friction velocity uk : 0.20502E+01 0.37616E+01 Dimensionless distance yplus : 0.51256E-01 0.94041E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62320E+01 456 0.10095E-01 0.99140E-06 0.43496E-02 c Velocity[X] 0.91978E-06 c Velocity[Y] 0.71621E-07 c Velocity[Z] 0.53183E-37 c Pressure 0.65007E-02 12 0.48807E-08 0.61909E-02 0.94740E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10452 0.99332 0.66405 0.66405 v Velocity[Y] -0.083684 0.083684 6.1751e-12 6.1751e-12 v Velocity[Z] -1.7002e-17 1.8578e-17 -5.3588e-21 -5.3588e-21 v ǁVelocityǁ 0.10452 0.99332 0.66413 0.66413 v Pressure 196.82 78975 39380 39380 v CourantNb 2.0888 19.839 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.13 2017.2 1573.4 1573.4 INSTANT 0.580000000E+01 TIME STEP NUMBER 58 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667003E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20447E+01 0.37606E+01 Friction velocity uk : 0.20447E+01 0.37606E+01 Dimensionless distance yplus : 0.51119E-01 0.94014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62324E+01 453 0.98050E-02 0.86760E-06 0.40684E-02 c Velocity[X] 0.80097E-06 c Velocity[Y] 0.66631E-07 c Velocity[Z] 0.42009E-37 c Pressure 0.63167E-02 11 0.96407E-08 0.59860E-02 0.87379E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10401 0.99372 0.66404 0.66404 v Velocity[Y] -0.082963 0.082963 2.1193e-11 2.1193e-11 v Velocity[Z] -1.6469e-17 1.7949e-17 -4.2913e-21 -4.2913e-21 v ǁVelocityǁ 0.10401 0.99372 0.66412 0.66412 v Pressure 196.99 79060 39414 39414 v CourantNb 2.0767 19.846 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.12 2017.2 1573.4 1573.4 INSTANT 0.590000000E+01 TIME STEP NUMBER 59 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667003E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20397E+01 0.37596E+01 Friction velocity uk : 0.20397E+01 0.37596E+01 Dimensionless distance yplus : 0.50992E-01 0.93989E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62328E+01 450 0.95202E-02 0.75494E-06 0.37946E-02 c Velocity[X] 0.68809E-06 c Velocity[Y] 0.66849E-07 c Velocity[Z] 0.37017E-37 c Pressure 0.61398E-02 11 0.91334E-08 0.57907E-02 0.80596E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10353 0.9941 0.66403 0.66403 v Velocity[Y] -0.082236 0.082236 1.5885e-12 1.5885e-12 v Velocity[Z] -1.6309e-17 1.7333e-17 -2.9671e-21 -2.9671e-21 v ǁVelocityǁ 0.10353 0.9941 0.66411 0.66411 v Pressure 197.14 79139 39446 39446 v CourantNb 2.0655 19.852 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.11 2017.2 1573.4 1573.4 INSTANT 0.600000000E+01 TIME STEP NUMBER 60 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20350E+01 0.37586E+01 Friction velocity uk : 0.20350E+01 0.37586E+01 Dimensionless distance yplus : 0.50875E-01 0.93964E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62331E+01 447 0.92444E-02 0.66179E-06 0.35524E-02 c Velocity[X] 0.59805E-06 c Velocity[Y] 0.63741E-07 c Velocity[Z] 0.34467E-37 c Pressure 0.59672E-02 11 0.86459E-08 0.56020E-02 0.74346E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10308 0.99446 0.66403 0.66403 v Velocity[Y] -0.081528 0.081528 -1.3287e-11 -1.3287e-11 v Velocity[Z] -1.6109e-17 1.68e-17 -3.6989e-21 -3.6989e-21 v ǁVelocityǁ 0.10308 0.99446 0.66411 0.66411 v Pressure 197.29 79213 39475 39475 v CourantNb 2.0546 19.858 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.1 2017.2 1573.4 1573.4 INSTANT 0.610000000E+01 TIME STEP NUMBER 61 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20306E+01 0.37576E+01 Friction velocity uk : 0.20306E+01 0.37576E+01 Dimensionless distance yplus : 0.50765E-01 0.93941E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62334E+01 444 0.89772E-02 0.58034E-06 0.33263E-02 c Velocity[X] 0.51905E-06 c Velocity[Y] 0.61297E-07 c Velocity[Z] 0.31998E-37 c Pressure 0.57999E-02 13 0.81114E-08 0.54208E-02 0.68586E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10267 0.99481 0.66402 0.66402 v Velocity[Y] -0.08083 0.08083 -4.5509e-10 -4.5509e-10 v Velocity[Z] -1.5868e-17 1.6291e-17 -4.2484e-21 -4.2484e-21 v ǁVelocityǁ 0.10267 0.99481 0.6641 0.6641 v Pressure 197.42 79281 39502 39502 v CourantNb 2.0449 19.863 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.09 2017.2 1573.4 1573.4 INSTANT 0.620000000E+01 TIME STEP NUMBER 62 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667006E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20266E+01 0.37567E+01 Friction velocity uk : 0.20266E+01 0.37567E+01 Dimensionless distance yplus : 0.50664E-01 0.93918E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62337E+01 441 0.87185E-02 0.51004E-06 0.31180E-02 c Velocity[X] 0.45122E-06 c Velocity[Y] 0.58816E-07 c Velocity[Z] 0.29577E-37 c Pressure 0.56374E-02 12 0.96771E-08 0.52463E-02 0.63277E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.1023 0.99513 0.66401 0.66401 v Velocity[Y] -0.080144 0.080144 -4.0388e-10 -4.0388e-10 v Velocity[Z] -1.5213e-17 1.5815e-17 -3.0819e-21 -3.0819e-21 v ǁVelocityǁ 0.1023 0.99513 0.66409 0.66409 v Pressure 197.54 79346 39527 39527 v CourantNb 2.0353 19.868 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.08 2017.2 1573.4 1573.4 INSTANT 0.630000000E+01 TIME STEP NUMBER 63 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667006E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20228E+01 0.37558E+01 Friction velocity uk : 0.20228E+01 0.37558E+01 Dimensionless distance yplus : 0.50571E-01 0.93896E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62339E+01 438 0.84682E-02 0.44914E-06 0.29257E-02 c Velocity[X] 0.39273E-06 c Velocity[Y] 0.56412E-07 c Velocity[Z] 0.25383E-37 c Pressure 0.54797E-02 12 0.91608E-08 0.50784E-02 0.58383E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10195 0.99544 0.664 0.664 v Velocity[Y] -0.079471 0.079471 -3.7055e-10 -3.7055e-10 v Velocity[Z] -1.4776e-17 1.5377e-17 -2.1672e-21 -2.1672e-21 v ǁVelocityǁ 0.10195 0.99544 0.66408 0.66408 v Pressure 197.65 79406 39549 39549 v CourantNb 2.0264 19.873 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.07 2017.2 1573.4 1573.4 INSTANT 0.640000000E+01 TIME STEP NUMBER 64 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667005E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20194E+01 0.37550E+01 Friction velocity uk : 0.20194E+01 0.37550E+01 Dimensionless distance yplus : 0.50485E-01 0.93875E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62342E+01 435 0.82259E-02 0.39634E-06 0.27481E-02 c Velocity[X] 0.34227E-06 c Velocity[Y] 0.54072E-07 c Velocity[Z] 0.22598E-37 c Pressure 0.53265E-02 12 0.86750E-08 0.49166E-02 0.53872E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10163 0.99573 0.664 0.664 v Velocity[Y] -0.07881 0.07881 -3.3524e-10 -3.3524e-10 v Velocity[Z] -1.483e-17 1.4988e-17 -2.5339e-21 -2.5339e-21 v ǁVelocityǁ 0.10163 0.99573 0.66407 0.66407 v Pressure 197.76 79462 39571 39571 v CourantNb 2.0183 19.877 13.415 13.415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.07 2017.2 1573.4 1573.4 INSTANT 0.650000000E+01 TIME STEP NUMBER 65 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667005E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20162E+01 0.37542E+01 Friction velocity uk : 0.20162E+01 0.37542E+01 Dimensionless distance yplus : 0.50406E-01 0.93855E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62344E+01 432 0.79908E-02 0.35143E-06 0.25875E-02 c Velocity[X] 0.30021E-06 c Velocity[Y] 0.51222E-07 c Velocity[Z] 0.23582E-37 c Pressure 0.51772E-02 12 0.82129E-08 0.47603E-02 0.49711E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10133 0.99599 0.66399 0.66399 v Velocity[Y] -0.078168 0.078168 -2.9922e-10 -2.9922e-10 v Velocity[Z] -1.4508e-17 1.4619e-17 -1.7936e-21 -1.7936e-21 v ǁVelocityǁ 0.10133 0.99599 0.66406 0.66406 v Pressure 197.86 79514 39590 39590 v CourantNb 2.01 19.881 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.06 2017.2 1573.4 1573.4 INSTANT 0.660000000E+01 TIME STEP NUMBER 66 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667004E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20132E+01 0.37534E+01 Friction velocity uk : 0.20132E+01 0.37534E+01 Dimensionless distance yplus : 0.50331E-01 0.93835E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62346E+01 429 0.77600E-02 0.31455E-06 0.24478E-02 c Velocity[X] 0.26735E-06 c Velocity[Y] 0.47196E-07 c Velocity[Z] 0.21816E-37 c Pressure 0.50304E-02 12 0.77769E-08 0.46081E-02 0.45873E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10105 0.99625 0.66398 0.66398 v Velocity[Y] -0.077559 0.077559 -2.6307e-10 -2.6307e-10 v Velocity[Z] -1.4515e-17 1.4279e-17 -3.9377e-21 -3.9377e-21 v ǁVelocityǁ 0.10105 0.99625 0.66406 0.66406 v Pressure 197.94 79563 39608 39608 v CourantNb 2.0028 19.885 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.06 2017.2 1573.4 1573.4 INSTANT 0.670000000E+01 TIME STEP NUMBER 67 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667004E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20105E+01 0.37527E+01 Friction velocity uk : 0.20105E+01 0.37527E+01 Dimensionless distance yplus : 0.50263E-01 0.93816E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62348E+01 426 0.75364E-02 0.27926E-06 0.23062E-02 c Velocity[X] 0.23404E-06 c Velocity[Y] 0.45220E-07 c Velocity[Z] 0.14933E-37 c Pressure 0.48882E-02 12 0.73677E-08 0.44616E-02 0.42333E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.1008 0.99651 0.66398 0.66398 v Velocity[Y] -0.07696 0.07696 -2.2679e-10 -2.2679e-10 v Velocity[Z] -1.4521e-17 1.3965e-17 -3.015e-21 -3.015e-21 v ǁVelocityǁ 0.1008 0.99651 0.66405 0.66405 v Pressure 198.03 79608 39625 39625 v CourantNb 1.9954 19.888 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.05 2017.2 1573.4 1573.4 INSTANT 0.680000000E+01 TIME STEP NUMBER 68 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667003E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20080E+01 0.37519E+01 Friction velocity uk : 0.20080E+01 0.37519E+01 Dimensionless distance yplus : 0.50200E-01 0.93798E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62350E+01 423 0.73199E-02 0.24853E-06 0.21755E-02 c Velocity[X] 0.20528E-06 c Velocity[Y] 0.43247E-07 c Velocity[Z] 0.12462E-37 c Pressure 0.47501E-02 12 0.69942E-08 0.43203E-02 0.39069E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10057 0.99675 0.66397 0.66397 v Velocity[Y] -0.076373 0.076373 -2.1016e-10 -2.1016e-10 v Velocity[Z] -1.4527e-17 1.3676e-17 -2.1883e-21 -2.1883e-21 v ǁVelocityǁ 0.10057 0.99675 0.66404 0.66404 v Pressure 198.1 79651 39640 39640 v CourantNb 1.9884 19.891 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.05 2017.2 1573.4 1573.4 INSTANT 0.690000000E+01 TIME STEP NUMBER 69 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667003E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20057E+01 0.37512E+01 Friction velocity uk : 0.20057E+01 0.37512E+01 Dimensionless distance yplus : 0.50143E-01 0.93781E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62352E+01 420 0.71068E-02 0.22374E-06 0.20641E-02 c Velocity[X] 0.18356E-06 c Velocity[Y] 0.40189E-07 c Velocity[Z] 0.14413E-37 c Pressure 0.46125E-02 11 0.96965E-08 0.41811E-02 0.36057E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10036 0.99698 0.66397 0.66397 v Velocity[Y] -0.075831 0.075831 -1.3138e-10 -1.3138e-10 v Velocity[Z] -1.4532e-17 1.3408e-17 -3.2963e-21 -3.2963e-21 v ǁVelocityǁ 0.10036 0.99698 0.66404 0.66404 v Pressure 198.17 79691 39654 39654 v CourantNb 1.9822 19.894 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.04 2017.2 1573.4 1573.4 INSTANT 0.700000000E+01 TIME STEP NUMBER 70 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20036E+01 0.37506E+01 Friction velocity uk : 0.20036E+01 0.37506E+01 Dimensionless distance yplus : 0.50090E-01 0.93764E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62353E+01 417 0.69058E-02 0.19733E-06 0.19383E-02 c Velocity[X] 0.15710E-06 c Velocity[Y] 0.40224E-07 c Velocity[Z] 0.14521E-37 c Pressure 0.44849E-02 11 0.92157E-08 0.40521E-02 0.33281E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.10016 0.99719 0.66396 0.66396 v Velocity[Y] -0.075242 0.075242 -1.2195e-10 -1.2195e-10 v Velocity[Z] -1.4417e-17 1.3148e-17 -2.5084e-21 -2.5084e-21 v ǁVelocityǁ 0.10016 0.99719 0.66403 0.66403 v Pressure 198.24 79728 39667 39667 v CourantNb 1.9755 19.897 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.04 2017.3 1573.4 1573.4 INSTANT 0.710000000E+01 TIME STEP NUMBER 71 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20016E+01 0.37499E+01 Friction velocity uk : 0.20016E+01 0.37499E+01 Dimensionless distance yplus : 0.50041E-01 0.93747E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62355E+01 414 0.67048E-02 0.17863E-06 0.18441E-02 c Velocity[X] 0.14143E-06 c Velocity[Y] 0.37202E-07 c Velocity[Z] 0.18539E-37 c Pressure 0.43561E-02 11 0.87534E-08 0.39234E-02 0.30720E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099982 0.99739 0.66395 0.66395 v Velocity[Y] -0.074702 0.074702 -8.4662e-11 -8.4662e-11 v Velocity[Z] -1.4541e-17 1.2929e-17 -4.8149e-22 -4.8149e-22 v ǁVelocityǁ 0.099982 0.99739 0.66402 0.66402 v Pressure 198.3 79763 39679 39679 v CourantNb 1.9693 19.9 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.03 2017.3 1573.4 1573.4 INSTANT 0.720000000E+01 TIME STEP NUMBER 72 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19998E+01 0.37493E+01 Friction velocity uk : 0.19998E+01 0.37493E+01 Dimensionless distance yplus : 0.49995E-01 0.93732E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62356E+01 411 0.65151E-02 0.15868E-06 0.17380E-02 c Velocity[X] 0.12199E-06 c Velocity[Y] 0.36698E-07 c Velocity[Z] 0.16209E-37 c Pressure 0.42354E-02 11 0.83881E-08 0.38030E-02 0.28358E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099817 0.99757 0.66395 0.66395 v Velocity[Y] -0.074147 0.074147 -5.8113e-11 -5.8113e-11 v Velocity[Z] -1.4546e-17 1.2724e-17 -2.1794e-21 -2.1794e-21 v ǁVelocityǁ 0.099818 0.99757 0.66402 0.66402 v Pressure 198.35 79796 39691 39691 v CourantNb 1.9639 19.902 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.03 2017.3 1573.4 1573.4 INSTANT 0.730000000E+01 TIME STEP NUMBER 73 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19982E+01 0.37487E+01 Friction velocity uk : 0.19982E+01 0.37487E+01 Dimensionless distance yplus : 0.49954E-01 0.93716E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62357E+01 408 0.63305E-02 0.14357E-06 0.16531E-02 c Velocity[X] 0.10923E-06 c Velocity[Y] 0.34342E-07 c Velocity[Z] 0.89339E-38 c Pressure 0.41160E-02 11 0.79084E-08 0.36848E-02 0.26180E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099668 0.99775 0.66394 0.66394 v Velocity[Y] -0.073705 0.073705 -1.3036e-11 -1.3036e-11 v Velocity[Z] -1.455e-17 1.2531e-17 -2.3997e-21 -2.3997e-21 v ǁVelocityǁ 0.099668 0.99775 0.66401 0.66401 v Pressure 198.4 79826 39701 39701 v CourantNb 1.9583 19.905 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.03 2017.3 1573.4 1573.4 INSTANT 0.740000000E+01 TIME STEP NUMBER 74 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19967E+01 0.37481E+01 Friction velocity uk : 0.19967E+01 0.37481E+01 Dimensionless distance yplus : 0.49917E-01 0.93702E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62359E+01 406 0.61497E-02 0.12978E-06 0.15716E-02 c Velocity[X] 0.97331E-07 c Velocity[Y] 0.32447E-07 c Velocity[Z] 0.18029E-37 c Pressure 0.39990E-02 11 0.75506E-08 0.35699E-02 0.24170E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099533 0.99791 0.66394 0.66394 v Velocity[Y] -0.073351 0.073351 1.5199e-11 1.5199e-11 v Velocity[Z] -1.4554e-17 1.2352e-17 -1.207e-21 -1.207e-21 v ǁVelocityǁ 0.099533 0.99791 0.66401 0.66401 v Pressure 198.45 79855 39710 39710 v CourantNb 1.9525 19.907 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.02 2017.3 1573.4 1573.4 INSTANT 0.750000000E+01 TIME STEP NUMBER 75 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19953E+01 0.37475E+01 Friction velocity uk : 0.19953E+01 0.37475E+01 Dimensionless distance yplus : 0.49883E-01 0.93688E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62360E+01 403 0.59705E-02 0.11773E-06 0.14968E-02 c Velocity[X] 0.87305E-07 c Velocity[Y] 0.30421E-07 c Velocity[Z] 0.16933E-37 c Pressure 0.38836E-02 11 0.71971E-08 0.34573E-02 0.22316E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09941 0.99807 0.66394 0.66394 v Velocity[Y] -0.073013 0.073013 4.4036e-11 4.4036e-11 v Velocity[Z] -1.4557e-17 1.2217e-17 -3.2933e-21 -3.2933e-21 v ǁVelocityǁ 0.09941 0.99807 0.664 0.664 v Pressure 198.49 79882 39719 39719 v CourantNb 1.9474 19.909 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.02 2017.3 1573.4 1573.4 INSTANT 0.760000000E+01 TIME STEP NUMBER 76 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19941E+01 0.37470E+01 Friction velocity uk : 0.19941E+01 0.37470E+01 Dimensionless distance yplus : 0.49852E-01 0.93675E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62361E+01 400 0.57969E-02 0.10660E-06 0.14243E-02 c Velocity[X] 0.77665E-07 c Velocity[Y] 0.28937E-07 c Velocity[Z] 0.18351E-37 c Pressure 0.37718E-02 11 0.68649E-08 0.33487E-02 0.20606E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0993 0.99821 0.66393 0.66393 v Velocity[Y] -0.072685 0.072685 7.083e-11 7.083e-11 v Velocity[Z] -1.456e-17 1.2219e-17 -1.1569e-21 -1.1569e-21 v ǁVelocityǁ 0.0993 0.99821 0.664 0.664 v Pressure 198.53 79907 39727 39727 v CourantNb 1.9429 19.911 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.02 2017.3 1573.4 1573.4 INSTANT 0.770000000E+01 TIME STEP NUMBER 77 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19930E+01 0.37465E+01 Friction velocity uk : 0.19930E+01 0.37465E+01 Dimensionless distance yplus : 0.49825E-01 0.93663E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62363E+01 397 0.56288E-02 0.96780E-07 0.13571E-02 c Velocity[X] 0.69296E-07 c Velocity[Y] 0.27484E-07 c Velocity[Z] 0.20815E-37 c Pressure 0.36632E-02 11 0.65521E-08 0.32439E-02 0.19029E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0992 0.99835 0.66393 0.66393 v Velocity[Y] -0.072368 0.072368 9.5547e-11 9.5547e-11 v Velocity[Z] -1.4563e-17 1.2222e-17 1.9296e-22 1.9296e-22 v ǁVelocityǁ 0.099201 0.99835 0.66399 0.66399 v Pressure 198.57 79931 39735 39735 v CourantNb 1.9386 19.913 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.02 2017.3 1573.4 1573.4 INSTANT 0.780000000E+01 TIME STEP NUMBER 78 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19920E+01 0.37460E+01 Friction velocity uk : 0.19920E+01 0.37460E+01 Dimensionless distance yplus : 0.49800E-01 0.93651E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62364E+01 394 0.54661E-02 0.88035E-07 0.12943E-02 c Velocity[X] 0.61937E-07 c Velocity[Y] 0.26098E-07 c Velocity[Z] 0.10351E-37 c Pressure 0.35578E-02 11 0.62434E-08 0.31427E-02 0.17573E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099111 0.99848 0.66392 0.66392 v Velocity[Y] -0.072059 0.072059 1.2138e-10 1.2138e-10 v Velocity[Z] -1.4566e-17 1.2224e-17 -2.0624e-21 -2.0624e-21 v ǁVelocityǁ 0.099111 0.99848 0.66399 0.66399 v Pressure 198.6 79953 39741 39741 v CourantNb 1.9335 19.915 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.02 2017.3 1573.4 1573.4 INSTANT 0.790000000E+01 TIME STEP NUMBER 79 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19911E+01 0.37455E+01 Friction velocity uk : 0.19911E+01 0.37455E+01 Dimensionless distance yplus : 0.49777E-01 0.93639E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62365E+01 391 0.53086E-02 0.80247E-07 0.12357E-02 c Velocity[X] 0.55474E-07 c Velocity[Y] 0.24773E-07 c Velocity[Z] 0.12544E-37 c Pressure 0.34555E-02 11 0.59659E-08 0.30450E-02 0.16230E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099031 0.9986 0.66392 0.66392 v Velocity[Y] -0.071759 0.071759 1.4212e-10 1.4212e-10 v Velocity[Z] -1.4568e-17 1.2226e-17 6.5365e-22 6.5365e-22 v ǁVelocityǁ 0.099032 0.9986 0.66398 0.66398 v Pressure 198.63 79974 39748 39748 v CourantNb 1.9286 19.917 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.01 2017.3 1573.4 1573.4 INSTANT 0.800000000E+01 TIME STEP NUMBER 80 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19903E+01 0.37451E+01 Friction velocity uk : 0.19903E+01 0.37451E+01 Dimensionless distance yplus : 0.49757E-01 0.93627E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62366E+01 388 0.51556E-02 0.73395E-07 0.11817E-02 c Velocity[X] 0.49999E-07 c Velocity[Y] 0.23396E-07 c Velocity[Z] 0.83789E-38 c Pressure 0.33559E-02 11 0.57021E-08 0.29502E-02 0.14991E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098958 0.99873 0.66391 0.66391 v Velocity[Y] -0.071468 0.071468 1.6138e-10 1.6138e-10 v Velocity[Z] -1.457e-17 1.2228e-17 -5.5164e-22 -5.5164e-22 v ǁVelocityǁ 0.098958 0.99873 0.66398 0.66398 v Pressure 198.66 79994 39754 39754 v CourantNb 1.9242 19.919 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.01 2017.3 1573.4 1573.4 INSTANT 0.810000000E+01 TIME STEP NUMBER 81 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19896E+01 0.37446E+01 Friction velocity uk : 0.19896E+01 0.37446E+01 Dimensionless distance yplus : 0.49739E-01 0.93616E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62367E+01 385 0.50032E-02 0.67919E-07 0.11367E-02 c Velocity[X] 0.46493E-07 c Velocity[Y] 0.21427E-07 c Velocity[Z] 0.92411E-38 c Pressure 0.32566E-02 11 0.54490E-08 0.28565E-02 0.13847E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09889 0.99885 0.66391 0.66391 v Velocity[Y] -0.071191 0.071191 1.7707e-10 1.7707e-10 v Velocity[Z] -1.4573e-17 1.223e-17 4.1122e-22 4.1122e-22 v ǁVelocityǁ 0.09889 0.99885 0.66397 0.66397 v Pressure 198.69 80013 39759 39759 v CourantNb 1.9205 19.92 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.01 2017.3 1573.4 1573.4 INSTANT 0.820000000E+01 TIME STEP NUMBER 82 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19889E+01 0.37442E+01 Friction velocity uk : 0.19889E+01 0.37442E+01 Dimensionless distance yplus : 0.49722E-01 0.93605E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62367E+01 382 0.48555E-02 0.62163E-07 0.10875E-02 c Velocity[X] 0.41794E-07 c Velocity[Y] 0.20369E-07 c Velocity[Z] 0.10588E-37 c Pressure 0.31604E-02 11 0.52093E-08 0.27660E-02 0.12791E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098829 0.99896 0.66391 0.66391 v Velocity[Y] -0.070906 0.070906 1.9165e-10 1.9165e-10 v Velocity[Z] -1.4574e-17 1.2231e-17 -6.3214e-22 -6.3214e-22 v ǁVelocityǁ 0.09883 0.99896 0.66397 0.66397 v Pressure 198.71 80030 39764 39764 v CourantNb 1.917 19.922 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.01 2017.3 1573.4 1573.4 INSTANT 0.830000000E+01 TIME STEP NUMBER 83 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19883E+01 0.37438E+01 Friction velocity uk : 0.19883E+01 0.37438E+01 Dimensionless distance yplus : 0.49706E-01 0.93595E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62368E+01 379 0.47118E-02 0.57053E-07 0.10418E-02 c Velocity[X] 0.37897E-07 c Velocity[Y] 0.19156E-07 c Velocity[Z] 0.21320E-37 c Pressure 0.30670E-02 11 0.49810E-08 0.26786E-02 0.11817E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098776 0.99907 0.6639 0.6639 v Velocity[Y] -0.070647 0.070647 2.0442e-10 2.0442e-10 v Velocity[Z] -1.4576e-17 1.2233e-17 1.0547e-21 1.0547e-21 v ǁVelocityǁ 0.098776 0.99907 0.66397 0.66397 v Pressure 198.74 80046 39769 39769 v CourantNb 1.9136 19.924 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.01 2017.3 1573.4 1573.4 INSTANT 0.840000000E+01 TIME STEP NUMBER 84 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19877E+01 0.37434E+01 Friction velocity uk : 0.19877E+01 0.37434E+01 Dimensionless distance yplus : 0.49693E-01 0.93585E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62369E+01 376 0.45724E-02 0.52404E-07 0.99845E-03 c Velocity[X] 0.34292E-07 c Velocity[Y] 0.18112E-07 c Velocity[Z] 0.13086E-37 c Pressure 0.29764E-02 11 0.47639E-08 0.25941E-02 0.10918E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098729 0.99917 0.6639 0.6639 v Velocity[Y] -0.070396 0.070396 2.1562e-10 2.1562e-10 v Velocity[Z] -1.4578e-17 1.2234e-17 -2.3508e-21 -2.3508e-21 v ǁVelocityǁ 0.09873 0.99917 0.66396 0.66396 v Pressure 198.76 80062 39773 39773 v CourantNb 1.9105 19.926 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802.01 2017.3 1573.4 1573.4 INSTANT 0.850000000E+01 TIME STEP NUMBER 85 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19873E+01 0.37430E+01 Friction velocity uk : 0.19873E+01 0.37430E+01 Dimensionless distance yplus : 0.49681E-01 0.93575E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62370E+01 373 0.44370E-02 0.48209E-07 0.95763E-03 c Velocity[X] 0.31087E-07 c Velocity[Y] 0.17122E-07 c Velocity[Z] 0.92366E-38 c Pressure 0.28884E-02 11 0.45574E-08 0.25124E-02 0.10088E-02 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098689 0.99927 0.6639 0.6639 v Velocity[Y] -0.070153 0.070153 2.2534e-10 2.2534e-10 v Velocity[Z] -1.4579e-17 1.2235e-17 1.5966e-22 1.5966e-22 v ǁVelocityǁ 0.098689 0.99927 0.66396 0.66396 v Pressure 198.78 80076 39777 39777 v CourantNb 1.9064 19.928 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.860000000E+01 TIME STEP NUMBER 86 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19868E+01 0.37426E+01 Friction velocity uk : 0.19868E+01 0.37426E+01 Dimensionless distance yplus : 0.49671E-01 0.93566E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62371E+01 371 0.43057E-02 0.44412E-07 0.91913E-03 c Velocity[X] 0.28230E-07 c Velocity[Y] 0.16182E-07 c Velocity[Z] 0.84727E-38 c Pressure 0.28031E-02 11 0.45373E-08 0.24335E-02 0.93227E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098654 0.99936 0.6639 0.6639 v Velocity[Y] -0.069917 0.069917 2.0644e-10 2.0644e-10 v Velocity[Z] -1.4581e-17 1.2237e-17 9.7803e-23 9.7803e-23 v ǁVelocityǁ 0.098654 0.99936 0.66396 0.66396 v Pressure 198.79 80090 39781 39781 v CourantNb 1.9025 19.93 13.416 13.416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.870000000E+01 TIME STEP NUMBER 87 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666996E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19865E+01 0.37423E+01 Friction velocity uk : 0.19865E+01 0.37423E+01 Dimensionless distance yplus : 0.49662E-01 0.93556E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62371E+01 368 0.41781E-02 0.40970E-07 0.88278E-03 c Velocity[X] 0.25680E-07 c Velocity[Y] 0.15289E-07 c Velocity[Z] 0.14386E-37 c Pressure 0.27203E-02 11 0.43451E-08 0.23572E-02 0.86162E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098624 0.99944 0.66389 0.66389 v Velocity[Y] -0.069689 0.069689 2.2037e-10 2.2037e-10 v Velocity[Z] -1.4466e-17 1.2182e-17 3.3004e-22 3.3004e-22 v ǁVelocityǁ 0.098625 0.99944 0.66395 0.66395 v Pressure 198.81 80103 39784 39784 v CourantNb 1.8989 19.931 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.880000000E+01 TIME STEP NUMBER 88 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666996E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19862E+01 0.37419E+01 Friction velocity uk : 0.19862E+01 0.37419E+01 Dimensionless distance yplus : 0.49655E-01 0.93548E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62372E+01 365 0.40544E-02 0.37843E-07 0.84842E-03 c Velocity[X] 0.23400E-07 c Velocity[Y] 0.14443E-07 c Velocity[Z] 0.16209E-37 c Pressure 0.26399E-02 11 0.41708E-08 0.22835E-02 0.79643E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098599 0.99952 0.66389 0.66389 v Velocity[Y] -0.069467 0.069467 2.2526e-10 2.2526e-10 v Velocity[Z] -1.4471e-17 1.2238e-17 1.0216e-21 1.0216e-21 v ǁVelocityǁ 0.0986 0.99952 0.66395 0.66395 v Pressure 198.82 80115 39787 39787 v CourantNb 1.8954 19.933 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.890000000E+01 TIME STEP NUMBER 89 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666996E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19859E+01 0.37416E+01 Friction velocity uk : 0.19859E+01 0.37416E+01 Dimensionless distance yplus : 0.49649E-01 0.93539E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62373E+01 362 0.39343E-02 0.34997E-07 0.81588E-03 c Velocity[X] 0.21356E-07 c Velocity[Y] 0.13641E-07 c Velocity[Z] 0.20566E-37 c Pressure 0.25619E-02 11 0.41663E-08 0.22122E-02 0.73626E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098579 0.9996 0.66389 0.66389 v Velocity[Y] -0.069252 0.069252 1.9878e-10 1.9878e-10 v Velocity[Z] -1.4584e-17 1.224e-17 2.4863e-21 2.4863e-21 v ǁVelocityǁ 0.098579 0.9996 0.66395 0.66395 v Pressure 198.84 80127 39790 39790 v CourantNb 1.8925 19.935 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.900000000E+01 TIME STEP NUMBER 90 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666994E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19857E+01 0.37412E+01 Friction velocity uk : 0.19857E+01 0.37412E+01 Dimensionless distance yplus : 0.49643E-01 0.93531E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62373E+01 359 0.38178E-02 0.32402E-07 0.78504E-03 c Velocity[X] 0.19521E-07 c Velocity[Y] 0.12881E-07 c Velocity[Z] 0.15509E-37 c Pressure 0.24863E-02 10 0.98672E-08 0.21432E-02 0.68073E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098562 0.99967 0.66388 0.66388 v Velocity[Y] -0.069043 0.069043 2.6362e-10 2.6362e-10 v Velocity[Z] -1.4585e-17 1.224e-17 1.8076e-21 1.8076e-21 v ǁVelocityǁ 0.098563 0.99967 0.66394 0.66394 v Pressure 198.85 80138 39792 39792 v CourantNb 1.8899 19.936 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.910000000E+01 TIME STEP NUMBER 91 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666994E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19856E+01 0.37409E+01 Friction velocity uk : 0.19856E+01 0.37409E+01 Dimensionless distance yplus : 0.49639E-01 0.93523E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62374E+01 356 0.37047E-02 0.30031E-07 0.75577E-03 c Velocity[X] 0.17871E-07 c Velocity[Y] 0.12161E-07 c Velocity[Z] 0.16026E-37 c Pressure 0.24128E-02 10 0.94722E-08 0.20765E-02 0.62949E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09855 0.99974 0.66388 0.66388 v Velocity[Y] -0.06884 0.06884 2.6897e-10 2.6897e-10 v Velocity[Z] -1.447e-17 1.2161e-17 2.0236e-21 2.0236e-21 v ǁVelocityǁ 0.09855 0.99974 0.66394 0.66394 v Pressure 198.86 80148 39795 39795 v CourantNb 1.8875 19.938 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.920000000E+01 TIME STEP NUMBER 92 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666994E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19854E+01 0.37406E+01 Friction velocity uk : 0.19854E+01 0.37406E+01 Dimensionless distance yplus : 0.49636E-01 0.93515E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62374E+01 353 0.35950E-02 0.27862E-07 0.72796E-03 c Velocity[X] 0.16383E-07 c Velocity[Y] 0.11479E-07 c Velocity[Z] 0.20370E-37 c Pressure 0.23416E-02 10 0.91004E-08 0.20120E-02 0.58220E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09854 0.9998 0.66388 0.66388 v Velocity[Y] -0.068643 0.068643 2.6918e-10 2.6918e-10 v Velocity[Z] -1.4467e-17 1.2241e-17 3.9437e-22 3.9437e-22 v ǁVelocityǁ 0.09854 0.9998 0.66394 0.66394 v Pressure 198.87 80158 39797 39797 v CourantNb 1.8852 19.939 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.930000000E+01 TIME STEP NUMBER 93 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666994E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19853E+01 0.37403E+01 Friction velocity uk : 0.19853E+01 0.37403E+01 Dimensionless distance yplus : 0.49634E-01 0.93507E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62375E+01 350 0.34886E-02 0.25874E-07 0.70150E-03 c Velocity[X] 0.15041E-07 c Velocity[Y] 0.10833E-07 c Velocity[Z] 0.24398E-37 c Pressure 0.22724E-02 11 0.89633E-08 0.19496E-02 0.53856E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098534 0.99986 0.66388 0.66388 v Velocity[Y] -0.068452 0.068452 1.881e-09 1.881e-09 v Velocity[Z] -1.4543e-17 1.2243e-17 2.7729e-21 2.7729e-21 v ǁVelocityǁ 0.098534 0.99986 0.66394 0.66394 v Pressure 198.88 80167 39799 39799 v CourantNb 1.883 19.94 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.940000000E+01 TIME STEP NUMBER 94 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19853E+01 0.37400E+01 Friction velocity uk : 0.19853E+01 0.37400E+01 Dimensionless distance yplus : 0.49632E-01 0.93500E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62375E+01 347 0.33853E-02 0.24049E-07 0.67630E-03 c Velocity[X] 0.13827E-07 c Velocity[Y] 0.10223E-07 c Velocity[Z] 0.17571E-37 c Pressure 0.22053E-02 11 0.85202E-08 0.18892E-02 0.49828E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09853 0.99991 0.66387 0.66387 v Velocity[Y] -0.068266 0.068266 1.816e-09 1.816e-09 v Velocity[Z] -1.4472e-17 1.2191e-17 1.9666e-21 1.9666e-21 v ǁVelocityǁ 0.098531 0.99991 0.66393 0.66393 v Pressure 198.89 80176 39801 39801 v CourantNb 1.881 19.942 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.950000000E+01 TIME STEP NUMBER 95 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19852E+01 0.37397E+01 Friction velocity uk : 0.19852E+01 0.37397E+01 Dimensionless distance yplus : 0.49631E-01 0.93493E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62376E+01 345 0.32851E-02 0.22371E-07 0.65228E-03 c Velocity[X] 0.12726E-07 c Velocity[Y] 0.96448E-08 c Velocity[Z] 0.94178E-38 c Pressure 0.21401E-02 11 0.81064E-08 0.18308E-02 0.46111E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098529 0.99997 0.66387 0.66387 v Velocity[Y] -0.068086 0.068086 1.7506e-09 1.7506e-09 v Velocity[Z] -1.4588e-17 1.2243e-17 2.3353e-21 2.3353e-21 v ǁVelocityǁ 0.09853 0.99997 0.66393 0.66393 v Pressure 198.9 80184 39803 39803 v CourantNb 1.879 19.943 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.960000000E+01 TIME STEP NUMBER 96 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19852E+01 0.37395E+01 Friction velocity uk : 0.19852E+01 0.37395E+01 Dimensionless distance yplus : 0.49631E-01 0.93486E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62376E+01 342 0.31879E-02 0.20826E-07 0.62935E-03 c Velocity[X] 0.11728E-07 c Velocity[Y] 0.90984E-08 c Velocity[Z] 0.12967E-37 c Pressure 0.20769E-02 11 0.77113E-08 0.17743E-02 0.42681E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098531 1 0.66387 0.66387 v Velocity[Y] -0.06791 0.06791 1.6847e-09 1.6847e-09 v Velocity[Z] -1.459e-17 1.2244e-17 -1.7527e-22 -1.7527e-22 v ǁVelocityǁ 0.098531 1 0.66393 0.66393 v Pressure 198.91 80192 39805 39805 v CourantNb 1.8772 19.945 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.970000000E+01 TIME STEP NUMBER 97 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19853E+01 0.37392E+01 Friction velocity uk : 0.19853E+01 0.37392E+01 Dimensionless distance yplus : 0.49631E-01 0.93480E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62377E+01 339 0.30936E-02 0.19402E-07 0.60745E-03 c Velocity[X] 0.10820E-07 c Velocity[Y] 0.85819E-08 c Velocity[Z] 0.14105E-37 c Pressure 0.20156E-02 11 0.73329E-08 0.17195E-02 0.39515E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098534 1.0001 0.66387 0.66387 v Velocity[Y] -0.06774 0.06774 1.6177e-09 1.6177e-09 v Velocity[Z] -1.459e-17 1.2245e-17 2.5675e-21 2.5675e-21 v ǁVelocityǁ 0.098534 1.0001 0.66393 0.66393 v Pressure 198.92 80199 39806 39806 v CourantNb 1.8751 19.946 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.980000000E+01 TIME STEP NUMBER 98 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19853E+01 0.37389E+01 Friction velocity uk : 0.19853E+01 0.37389E+01 Dimensionless distance yplus : 0.49632E-01 0.93473E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62377E+01 336 0.30021E-02 0.18087E-07 0.58650E-03 c Velocity[X] 0.99937E-08 c Velocity[Y] 0.80936E-08 c Velocity[Z] 0.15385E-37 c Pressure 0.19560E-02 11 0.69717E-08 0.16666E-02 0.36593E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09854 1.0001 0.66387 0.66387 v Velocity[Y] -0.067575 0.067575 1.5508e-09 1.5508e-09 v Velocity[Z] -1.4591e-17 1.2245e-17 2.5895e-21 2.5895e-21 v ǁVelocityǁ 0.09854 1.0001 0.66392 0.66392 v Pressure 198.92 80206 39807 39807 v CourantNb 1.8726 19.947 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 802 2017.3 1573.4 1573.4 INSTANT 0.990000000E+01 TIME STEP NUMBER 99 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19853E+01 0.37387E+01 Friction velocity uk : 0.19853E+01 0.37387E+01 Dimensionless distance yplus : 0.49634E-01 0.93467E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62378E+01 333 0.29133E-02 0.16872E-07 0.56645E-03 c Velocity[X] 0.92398E-08 c Velocity[Y] 0.76322E-08 c Velocity[Z] 0.37167E-37 c Pressure 0.18982E-02 11 0.66271E-08 0.16153E-02 0.33896E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098547 1.0002 0.66386 0.66386 v Velocity[Y] -0.067414 0.067414 1.4846e-09 1.4846e-09 v Velocity[Z] -1.4591e-17 1.2246e-17 2.5224e-21 2.5224e-21 v ǁVelocityǁ 0.098547 1.0002 0.66392 0.66392 v Pressure 198.93 80213 39809 39809 v CourantNb 1.8703 19.948 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.100000000E+02 TIME STEP NUMBER 100 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19854E+01 0.37385E+01 Friction velocity uk : 0.19854E+01 0.37385E+01 Dimensionless distance yplus : 0.49635E-01 0.93461E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62378E+01 330 0.28271E-02 0.15747E-07 0.54724E-03 c Velocity[X] 0.85511E-08 c Velocity[Y] 0.71963E-08 c Velocity[Z] 0.18250E-37 c Pressure 0.18422E-02 11 0.63033E-08 0.15657E-02 0.31407E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098555 1.0002 0.66386 0.66386 v Velocity[Y] -0.067258 0.067258 1.4205e-09 1.4205e-09 v Velocity[Z] -1.4592e-17 1.2246e-17 1.3348e-21 1.3348e-21 v ǁVelocityǁ 0.098556 1.0002 0.66392 0.66392 v Pressure 198.94 80219 39810 39810 v CourantNb 1.868 19.949 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.101000000E+02 TIME STEP NUMBER 101 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19855E+01 0.37382E+01 Friction velocity uk : 0.19855E+01 0.37382E+01 Dimensionless distance yplus : 0.49638E-01 0.93456E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62378E+01 328 0.27435E-02 0.14706E-07 0.52883E-03 c Velocity[X] 0.79210E-08 c Velocity[Y] 0.67845E-08 c Velocity[Z] 0.21576E-37 c Pressure 0.17877E-02 11 0.59848E-08 0.15176E-02 0.29110E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098565 1.0002 0.66386 0.66386 v Velocity[Y] -0.067107 0.067107 1.3538e-09 1.3538e-09 v Velocity[Z] -1.4592e-17 1.2246e-17 3.9949e-21 3.9949e-21 v ǁVelocityǁ 0.098566 1.0002 0.66392 0.66392 v Pressure 198.94 80225 39811 39811 v CourantNb 1.8658 19.95 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.102000000E+02 TIME STEP NUMBER 102 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19856E+01 0.37380E+01 Friction velocity uk : 0.19856E+01 0.37380E+01 Dimensionless distance yplus : 0.49640E-01 0.93450E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62379E+01 325 0.26624E-02 0.13740E-07 0.51116E-03 c Velocity[X] 0.73439E-08 c Velocity[Y] 0.63957E-08 c Velocity[Z] 0.22599E-37 c Pressure 0.17349E-02 11 0.56847E-08 0.14711E-02 0.26990E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098577 1.0003 0.66386 0.66386 v Velocity[Y] -0.06696 0.06696 1.2896e-09 1.2896e-09 v Velocity[Z] -1.4593e-17 1.2247e-17 3.7715e-21 3.7715e-21 v ǁVelocityǁ 0.098577 1.0003 0.66392 0.66392 v Pressure 198.95 80231 39812 39812 v CourantNb 1.8638 19.951 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.103000000E+02 TIME STEP NUMBER 103 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19857E+01 0.37378E+01 Friction velocity uk : 0.19857E+01 0.37378E+01 Dimensionless distance yplus : 0.49643E-01 0.93445E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62379E+01 322 0.25837E-02 0.12843E-07 0.49420E-03 c Velocity[X] 0.68145E-08 c Velocity[Y] 0.60285E-08 c Velocity[Z] 0.14318E-37 c Pressure 0.16836E-02 10 0.99243E-08 0.14260E-02 0.25033E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098589 1.0003 0.66386 0.66386 v Velocity[Y] -0.066818 0.066818 1.2964e-09 1.2964e-09 v Velocity[Z] -1.4593e-17 1.2247e-17 5.4125e-21 5.4125e-21 v ǁVelocityǁ 0.098589 1.0003 0.66391 0.66391 v Pressure 198.95 80237 39813 39813 v CourantNb 1.8618 19.952 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.104000000E+02 TIME STEP NUMBER 104 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19858E+01 0.37376E+01 Friction velocity uk : 0.19858E+01 0.37376E+01 Dimensionless distance yplus : 0.49646E-01 0.93439E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62379E+01 319 0.25074E-02 0.12010E-07 0.47790E-03 c Velocity[X] 0.63280E-08 c Velocity[Y] 0.56819E-08 c Velocity[Z] 0.33490E-37 c Pressure 0.16339E-02 10 0.94065E-08 0.13824E-02 0.23227E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098603 1.0003 0.66386 0.66386 v Velocity[Y] -0.066679 0.066679 1.2332e-09 1.2332e-09 v Velocity[Z] -1.4474e-17 1.2191e-17 9.3483e-22 9.3483e-22 v ǁVelocityǁ 0.098603 1.0003 0.66391 0.66391 v Pressure 198.96 80242 39814 39814 v CourantNb 1.8599 19.953 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.105000000E+02 TIME STEP NUMBER 105 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19860E+01 0.37374E+01 Friction velocity uk : 0.19860E+01 0.37374E+01 Dimensionless distance yplus : 0.49649E-01 0.93434E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62380E+01 316 0.24333E-02 0.11235E-07 0.46223E-03 c Velocity[X] 0.58807E-08 c Velocity[Y] 0.53547E-08 c Velocity[Z] 0.24170E-37 c Pressure 0.15856E-02 10 0.89156E-08 0.13402E-02 0.21560E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098617 1.0004 0.66386 0.66386 v Velocity[Y] -0.066545 0.066545 1.1731e-09 1.1731e-09 v Velocity[Z] -1.4592e-17 1.2247e-17 3.3038e-21 3.3038e-21 v ǁVelocityǁ 0.098617 1.0004 0.66391 0.66391 v Pressure 198.96 80247 39815 39815 v CourantNb 1.8581 19.954 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.106000000E+02 TIME STEP NUMBER 106 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19861E+01 0.37372E+01 Friction velocity uk : 0.19861E+01 0.37372E+01 Dimensionless distance yplus : 0.49653E-01 0.93429E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62380E+01 314 0.23614E-02 0.10515E-07 0.44716E-03 c Velocity[X] 0.54687E-08 c Velocity[Y] 0.50459E-08 c Velocity[Z] 0.16216E-37 c Pressure 0.15387E-02 10 0.88041E-08 0.12993E-02 0.20021E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098632 1.0004 0.66385 0.66385 v Velocity[Y] -0.066414 0.066414 1.2627e-09 1.2627e-09 v Velocity[Z] -1.4594e-17 1.2248e-17 2.3411e-21 2.3411e-21 v ǁVelocityǁ 0.098632 1.0004 0.66391 0.66391 v Pressure 198.96 80252 39815 39815 v CourantNb 1.8564 19.955 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.107000000E+02 TIME STEP NUMBER 107 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19863E+01 0.37370E+01 Friction velocity uk : 0.19863E+01 0.37370E+01 Dimensionless distance yplus : 0.49657E-01 0.93425E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62380E+01 311 0.22916E-02 0.98435E-08 0.43265E-03 c Velocity[X] 0.50889E-08 c Velocity[Y] 0.47545E-08 c Velocity[Z] 0.19472E-37 c Pressure 0.14932E-02 10 0.83725E-08 0.12596E-02 0.18601E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098648 1.0004 0.66385 0.66385 v Velocity[Y] -0.066287 0.066287 1.2057e-09 1.2057e-09 v Velocity[Z] -1.4478e-17 1.2193e-17 5.8976e-23 5.8976e-23 v ǁVelocityǁ 0.098648 1.0004 0.66391 0.66391 v Pressure 198.97 80256 39816 39816 v CourantNb 1.8549 19.956 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.108000000E+02 TIME STEP NUMBER 108 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19864E+01 0.37368E+01 Friction velocity uk : 0.19864E+01 0.37368E+01 Dimensionless distance yplus : 0.49661E-01 0.93420E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62380E+01 308 0.22239E-02 0.92181E-08 0.41868E-03 c Velocity[X] 0.47384E-08 c Velocity[Y] 0.44796E-08 c Velocity[Z] 0.24662E-37 c Pressure 0.14491E-02 10 0.79632E-08 0.12212E-02 0.17290E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098664 1.0004 0.66385 0.66385 v Velocity[Y] -0.066164 0.066164 1.1493e-09 1.1493e-09 v Velocity[Z] -1.4593e-17 1.2246e-17 2.6215e-21 2.6215e-21 v ǁVelocityǁ 0.098664 1.0004 0.66391 0.66391 v Pressure 198.97 80260 39817 39817 v CourantNb 1.8537 19.956 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.109000000E+02 TIME STEP NUMBER 109 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19866E+01 0.37366E+01 Friction velocity uk : 0.19866E+01 0.37366E+01 Dimensionless distance yplus : 0.49665E-01 0.93416E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62381E+01 305 0.21582E-02 0.86349E-08 0.40522E-03 c Velocity[X] 0.44146E-08 c Velocity[Y] 0.42203E-08 c Velocity[Z] 0.14091E-37 c Pressure 0.14063E-02 10 0.75771E-08 0.11841E-02 0.16080E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098681 1.0005 0.66385 0.66385 v Velocity[Y] -0.066045 0.066045 1.0947e-09 1.0947e-09 v Velocity[Z] -1.4594e-17 1.2248e-17 2.8603e-21 2.8603e-21 v ǁVelocityǁ 0.098681 1.0005 0.6639 0.6639 v Pressure 198.97 80264 39817 39817 v CourantNb 1.8525 19.957 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.110000000E+02 TIME STEP NUMBER 110 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19868E+01 0.37365E+01 Friction velocity uk : 0.19868E+01 0.37365E+01 Dimensionless distance yplus : 0.49669E-01 0.93411E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62381E+01 303 0.20945E-02 0.80908E-08 0.39225E-03 c Velocity[X] 0.41151E-08 c Velocity[Y] 0.39757E-08 c Velocity[Z] 0.12812E-37 c Pressure 0.13647E-02 10 0.72126E-08 0.11480E-02 0.14963E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098698 1.0005 0.66385 0.66385 v Velocity[Y] -0.065929 0.065929 1.042e-09 1.042e-09 v Velocity[Z] -1.4595e-17 1.2248e-17 3.6732e-21 3.6732e-21 v ǁVelocityǁ 0.098699 1.0005 0.6639 0.6639 v Pressure 198.97 80268 39818 39818 v CourantNb 1.8514 19.958 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.111000000E+02 TIME STEP NUMBER 111 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19869E+01 0.37363E+01 Friction velocity uk : 0.19869E+01 0.37363E+01 Dimensionless distance yplus : 0.49674E-01 0.93407E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62381E+01 300 0.20326E-02 0.75830E-08 0.37973E-03 c Velocity[X] 0.38379E-08 c Velocity[Y] 0.37451E-08 c Velocity[Z] 0.27045E-37 c Pressure 0.13243E-02 10 0.68816E-08 0.11131E-02 0.13932E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098716 1.0005 0.66385 0.66385 v Velocity[Y] -0.065817 0.065817 9.8231e-10 9.8231e-10 v Velocity[Z] -1.4595e-17 1.2249e-17 2.253e-21 2.253e-21 v ǁVelocityǁ 0.098716 1.0005 0.6639 0.6639 v Pressure 198.98 80272 39818 39818 v CourantNb 1.8503 19.959 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.112000000E+02 TIME STEP NUMBER 112 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19871E+01 0.37361E+01 Friction velocity uk : 0.19871E+01 0.37361E+01 Dimensionless distance yplus : 0.49678E-01 0.93403E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62381E+01 297 0.19726E-02 0.71086E-08 0.36767E-03 c Velocity[X] 0.35811E-08 c Velocity[Y] 0.35275E-08 c Velocity[Z] 0.25064E-37 c Pressure 0.12852E-02 10 0.65387E-08 0.10793E-02 0.12980E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098734 1.0005 0.66385 0.66385 v Velocity[Y] -0.065708 0.065708 9.4321e-10 9.4321e-10 v Velocity[Z] -1.4595e-17 1.2249e-17 3.5392e-21 3.5392e-21 v ǁVelocityǁ 0.098734 1.0005 0.6639 0.6639 v Pressure 198.98 80276 39819 39819 v CourantNb 1.8493 19.959 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.113000000E+02 TIME STEP NUMBER 113 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19873E+01 0.37360E+01 Friction velocity uk : 0.19873E+01 0.37360E+01 Dimensionless distance yplus : 0.49683E-01 0.93399E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62382E+01 295 0.19144E-02 0.66654E-08 0.35602E-03 c Velocity[X] 0.33429E-08 c Velocity[Y] 0.33224E-08 c Velocity[Z] 0.21312E-37 c Pressure 0.12472E-02 10 0.62270E-08 0.10466E-02 0.12102E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098752 1.0005 0.66384 0.66384 v Velocity[Y] -0.065602 0.065602 9.036e-10 9.036e-10 v Velocity[Z] -1.4595e-17 1.2249e-17 3.4501e-21 3.4501e-21 v ǁVelocityǁ 0.098753 1.0005 0.6639 0.6639 v Pressure 198.98 80279 39819 39819 v CourantNb 1.8484 19.96 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.114000000E+02 TIME STEP NUMBER 114 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19875E+01 0.37358E+01 Friction velocity uk : 0.19875E+01 0.37358E+01 Dimensionless distance yplus : 0.49687E-01 0.93396E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62382E+01 292 0.18578E-02 0.62511E-08 0.34477E-03 c Velocity[X] 0.31220E-08 c Velocity[Y] 0.31291E-08 c Velocity[Z] 0.14624E-37 c Pressure 0.12103E-02 10 0.59489E-08 0.10148E-02 0.11290E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098771 1.0006 0.66384 0.66384 v Velocity[Y] -0.065499 0.065499 8.499e-10 8.499e-10 v Velocity[Z] -1.4596e-17 1.2249e-17 3.4038e-21 3.4038e-21 v ǁVelocityǁ 0.098771 1.0006 0.6639 0.6639 v Pressure 198.98 80282 39819 39819 v CourantNb 1.8475 19.961 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.115000000E+02 TIME STEP NUMBER 115 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19877E+01 0.37357E+01 Friction velocity uk : 0.19877E+01 0.37357E+01 Dimensionless distance yplus : 0.49692E-01 0.93392E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62382E+01 289 0.18030E-02 0.58636E-08 0.33392E-03 c Velocity[X] 0.29168E-08 c Velocity[Y] 0.29468E-08 c Velocity[Z] 0.10567E-37 c Pressure 0.11745E-02 9 0.97982E-08 0.98406E-03 0.10541E-03 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098789 1.0006 0.66384 0.66384 v Velocity[Y] -0.0654 0.0654 7.8361e-10 7.8361e-10 v Velocity[Z] -1.4595e-17 1.2249e-17 1.2666e-21 1.2666e-21 v ǁVelocityǁ 0.09879 1.0006 0.6639 0.6639 v Pressure 198.98 80285 39820 39820 v CourantNb 1.8466 19.961 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.116000000E+02 TIME STEP NUMBER 116 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666979E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19879E+01 0.37355E+01 Friction velocity uk : 0.19879E+01 0.37355E+01 Dimensionless distance yplus : 0.49696E-01 0.93388E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62382E+01 287 0.17498E-02 0.55011E-08 0.32343E-03 c Velocity[X] 0.27261E-08 c Velocity[Y] 0.27750E-08 c Velocity[Z] 0.17231E-37 c Pressure 0.11397E-02 10 0.90662E-08 0.95425E-03 0.98487E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098808 1.0006 0.66384 0.66384 v Velocity[Y] -0.065303 0.065303 1.3657e-09 1.3657e-09 v Velocity[Z] -1.448e-17 1.2156e-17 4.3734e-21 4.3734e-21 v ǁVelocityǁ 0.098808 1.0006 0.6639 0.6639 v Pressure 198.99 80288 39820 39820 v CourantNb 1.8458 19.962 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.117000000E+02 TIME STEP NUMBER 117 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666975E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19880E+01 0.37354E+01 Friction velocity uk : 0.19880E+01 0.37354E+01 Dimensionless distance yplus : 0.49701E-01 0.93385E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62382E+01 284 0.16981E-02 0.51617E-08 0.31330E-03 c Velocity[X] 0.25487E-08 c Velocity[Y] 0.26130E-08 c Velocity[Z] 0.15715E-37 c Pressure 0.11060E-02 10 0.86166E-08 0.92536E-03 0.92094E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098827 1.0006 0.66384 0.66384 v Velocity[Y] -0.065209 0.065209 1.2455e-09 1.2455e-09 v Velocity[Z] -1.4596e-17 1.2255e-17 3.5327e-21 3.5327e-21 v ǁVelocityǁ 0.098827 1.0006 0.66389 0.66389 v Pressure 198.99 80291 39820 39820 v CourantNb 1.845 19.963 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.118000000E+02 TIME STEP NUMBER 118 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666976E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19882E+01 0.37353E+01 Friction velocity uk : 0.19882E+01 0.37353E+01 Dimensionless distance yplus : 0.49706E-01 0.93382E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62383E+01 282 0.16480E-02 0.48441E-08 0.30350E-03 c Velocity[X] 0.23837E-08 c Velocity[Y] 0.24604E-08 c Velocity[Z] 0.14555E-37 c Pressure 0.10733E-02 10 0.81927E-08 0.89737E-03 0.86189E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098845 1.0006 0.66384 0.66384 v Velocity[Y] -0.065118 0.065118 1.1331e-09 1.1331e-09 v Velocity[Z] -1.4596e-17 1.225e-17 4.3912e-21 4.3912e-21 v ǁVelocityǁ 0.098846 1.0006 0.66389 0.66389 v Pressure 198.99 80294 39821 39821 v CourantNb 1.8442 19.963 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.119000000E+02 TIME STEP NUMBER 119 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666977E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19884E+01 0.37351E+01 Friction velocity uk : 0.19884E+01 0.37351E+01 Dimensionless distance yplus : 0.49711E-01 0.93378E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62383E+01 279 0.15993E-02 0.45491E-08 0.29411E-03 c Velocity[X] 0.22329E-08 c Velocity[Y] 0.23162E-08 c Velocity[Z] 0.24401E-37 c Pressure 0.10415E-02 10 0.77942E-08 0.87024E-03 0.80733E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098864 1.0006 0.66384 0.66384 v Velocity[Y] -0.06503 0.06503 1.0282e-09 1.0282e-09 v Velocity[Z] -1.4596e-17 1.225e-17 3.2044e-21 3.2044e-21 v ǁVelocityǁ 0.098864 1.0006 0.66389 0.66389 v Pressure 198.99 80297 39821 39821 v CourantNb 1.8435 19.964 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.120000000E+02 TIME STEP NUMBER 120 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666978E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19886E+01 0.37350E+01 Friction velocity uk : 0.19886E+01 0.37350E+01 Dimensionless distance yplus : 0.49715E-01 0.93375E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62383E+01 276 0.15521E-02 0.42681E-08 0.28489E-03 c Velocity[X] 0.20869E-08 c Velocity[Y] 0.21812E-08 c Velocity[Z] 0.12223E-37 c Pressure 0.10107E-02 10 0.74166E-08 0.84394E-03 0.75689E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098883 1.0006 0.66384 0.66384 v Velocity[Y] -0.064944 0.064944 9.3053e-10 9.3053e-10 v Velocity[Z] -1.4596e-17 1.225e-17 4.7157e-21 4.7157e-21 v ǁVelocityǁ 0.098883 1.0006 0.66389 0.66389 v Pressure 198.99 80299 39821 39821 v CourantNb 1.8428 19.964 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.121000000E+02 TIME STEP NUMBER 121 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666979E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19888E+01 0.37349E+01 Friction velocity uk : 0.19888E+01 0.37349E+01 Dimensionless distance yplus : 0.49720E-01 0.93372E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62383E+01 274 0.15063E-02 0.40069E-08 0.27603E-03 c Velocity[X] 0.19534E-08 c Velocity[Y] 0.20535E-08 c Velocity[Z] 0.14322E-37 c Pressure 0.98081E-03 10 0.70600E-08 0.81845E-03 0.71026E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098901 1.0007 0.66384 0.66384 v Velocity[Y] -0.064861 0.064861 8.3988e-10 8.3988e-10 v Velocity[Z] -1.4596e-17 1.225e-17 3.351e-21 3.351e-21 v ǁVelocityǁ 0.098902 1.0007 0.66389 0.66389 v Pressure 198.99 80302 39821 39821 v CourantNb 1.8422 19.965 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.122000000E+02 TIME STEP NUMBER 122 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666980E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19890E+01 0.37348E+01 Friction velocity uk : 0.19890E+01 0.37348E+01 Dimensionless distance yplus : 0.49725E-01 0.93369E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62383E+01 271 0.14618E-02 0.37623E-08 0.26747E-03 c Velocity[X] 0.18291E-08 c Velocity[Y] 0.19332E-08 c Velocity[Z] 0.17894E-37 c Pressure 0.95177E-03 10 0.67230E-08 0.79375E-03 0.66713E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09892 1.0007 0.66384 0.66384 v Velocity[Y] -0.064781 0.064781 7.5582e-10 7.5582e-10 v Velocity[Z] -1.4596e-17 1.225e-17 5.2661e-21 5.2661e-21 v ǁVelocityǁ 0.09892 1.0007 0.66389 0.66389 v Pressure 198.99 80304 39822 39822 v CourantNb 1.8415 19.965 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.123000000E+02 TIME STEP NUMBER 123 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666980E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19892E+01 0.37347E+01 Friction velocity uk : 0.19892E+01 0.37347E+01 Dimensionless distance yplus : 0.49729E-01 0.93367E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62383E+01 269 0.14187E-02 0.35329E-08 0.25919E-03 c Velocity[X] 0.17130E-08 c Velocity[Y] 0.18199E-08 c Velocity[Z] 0.34766E-37 c Pressure 0.92360E-03 10 0.62680E-08 0.76980E-03 0.62724E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098938 1.0007 0.66384 0.66384 v Velocity[Y] -0.064703 0.064703 5.9373e-10 5.9373e-10 v Velocity[Z] -1.4596e-17 1.225e-17 2.8152e-21 2.8152e-21 v ǁVelocityǁ 0.098938 1.0007 0.66389 0.66389 v Pressure 198.99 80306 39822 39822 v CourantNb 1.8409 19.966 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.124000000E+02 TIME STEP NUMBER 124 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666981E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19894E+01 0.37346E+01 Friction velocity uk : 0.19894E+01 0.37346E+01 Dimensionless distance yplus : 0.49734E-01 0.93364E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62384E+01 267 0.13768E-02 0.33178E-08 0.25118E-03 c Velocity[X] 0.16046E-08 c Velocity[Y] 0.17132E-08 c Velocity[Z] 0.13058E-37 c Pressure 0.89626E-03 10 0.61031E-08 0.74658E-03 0.59032E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098956 1.0007 0.66383 0.66383 v Velocity[Y] -0.064627 0.064627 6.0625e-10 6.0625e-10 v Velocity[Z] -1.4596e-17 1.225e-17 3.1183e-21 3.1183e-21 v ǁVelocityǁ 0.098957 1.0007 0.66389 0.66389 v Pressure 199 80308 39822 39822 v CourantNb 1.8404 19.966 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.125000000E+02 TIME STEP NUMBER 125 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19895E+01 0.37344E+01 Friction velocity uk : 0.19895E+01 0.37344E+01 Dimensionless distance yplus : 0.49738E-01 0.93361E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 125, Physical time 0.12500E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 125: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62384E+01 264 0.13361E-02 0.31161E-08 0.24342E-03 c Velocity[X] 0.15035E-08 c Velocity[Y] 0.16126E-08 c Velocity[Z] 0.14179E-37 c Pressure 0.86972E-03 9 0.98614E-08 0.72408E-03 0.55613E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.098974 1.0007 0.66383 0.66383 v Velocity[Y] -0.064553 0.064553 6.1325e-10 6.1325e-10 v Velocity[Z] -1.4596e-17 1.225e-17 3.7279e-21 3.7279e-21 v ǁVelocityǁ 0.098974 1.0007 0.66389 0.66389 v Pressure 199 80310 39822 39822 v CourantNb 1.8398 19.967 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.126000000E+02 TIME STEP NUMBER 126 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19897E+01 0.37343E+01 Friction velocity uk : 0.19897E+01 0.37343E+01 Dimensionless distance yplus : 0.49743E-01 0.93359E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62384E+01 262 0.12967E-02 0.29269E-08 0.23592E-03 c Velocity[X] 0.14090E-08 c Velocity[Y] 0.15179E-08 c Velocity[Z] 0.12351E-37 c Pressure 0.84397E-03 9 0.94431E-08 0.70227E-03 0.52446E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09899 1.0007 0.66383 0.66383 v Velocity[Y] -0.064482 0.064482 5.3737e-10 5.3737e-10 v Velocity[Z] -1.4479e-17 1.2193e-17 3.0951e-21 3.0951e-21 v ǁVelocityǁ 0.09899 1.0007 0.66389 0.66389 v Pressure 199 80312 39822 39822 v CourantNb 1.8393 19.967 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.127000000E+02 TIME STEP NUMBER 127 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19899E+01 0.37342E+01 Friction velocity uk : 0.19899E+01 0.37342E+01 Dimensionless distance yplus : 0.49747E-01 0.93356E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62384E+01 259 0.12584E-02 0.27494E-08 0.22865E-03 c Velocity[X] 0.13207E-08 c Velocity[Y] 0.14287E-08 c Velocity[Z] 0.17165E-37 c Pressure 0.81898E-03 9 0.90446E-08 0.68112E-03 0.49510E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099006 1.0007 0.66383 0.66383 v Velocity[Y] -0.064413 0.064413 4.6757e-10 4.6757e-10 v Velocity[Z] -1.4601e-17 1.2249e-17 3.1709e-21 3.1709e-21 v ǁVelocityǁ 0.099006 1.0007 0.66389 0.66389 v Pressure 199 80314 39823 39823 v CourantNb 1.8388 19.968 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.128000000E+02 TIME STEP NUMBER 128 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19900E+01 0.37341E+01 Friction velocity uk : 0.19900E+01 0.37341E+01 Dimensionless distance yplus : 0.49751E-01 0.93354E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62384E+01 257 0.12213E-02 0.25829E-08 0.22162E-03 c Velocity[X] 0.12382E-08 c Velocity[Y] 0.13448E-08 c Velocity[Z] 0.17649E-37 c Pressure 0.79472E-03 9 0.86637E-08 0.66061E-03 0.46788E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099021 1.0007 0.66383 0.66383 v Velocity[Y] -0.064345 0.064345 4.0379e-10 4.0379e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.5383e-21 4.5383e-21 v ǁVelocityǁ 0.099022 1.0007 0.66388 0.66388 v Pressure 199 80316 39823 39823 v CourantNb 1.8384 19.968 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.129000000E+02 TIME STEP NUMBER 129 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19902E+01 0.37341E+01 Friction velocity uk : 0.19902E+01 0.37341E+01 Dimensionless distance yplus : 0.49755E-01 0.93351E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62384E+01 255 0.11852E-02 0.24266E-08 0.21481E-03 c Velocity[X] 0.11610E-08 c Velocity[Y] 0.12657E-08 c Velocity[Z] 0.13186E-37 c Pressure 0.77118E-03 9 0.83025E-08 0.64074E-03 0.44262E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099037 1.0007 0.66383 0.66383 v Velocity[Y] -0.06428 0.06428 3.4766e-10 3.4766e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.4926e-21 3.4926e-21 v ǁVelocityǁ 0.099037 1.0007 0.66388 0.66388 v Pressure 199 80318 39823 39823 v CourantNb 1.8379 19.968 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.130000000E+02 TIME STEP NUMBER 130 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19903E+01 0.37340E+01 Friction velocity uk : 0.19903E+01 0.37340E+01 Dimensionless distance yplus : 0.49759E-01 0.93349E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62384E+01 252 0.11502E-02 0.22800E-08 0.20822E-03 c Velocity[X] 0.10888E-08 c Velocity[Y] 0.11912E-08 c Velocity[Z] 0.13277E-37 c Pressure 0.74834E-03 9 0.79531E-08 0.62146E-03 0.41915E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099052 1.0007 0.66383 0.66383 v Velocity[Y] -0.064217 0.064217 2.9177e-10 2.9177e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3323e-21 4.3323e-21 v ǁVelocityǁ 0.099052 1.0007 0.66388 0.66388 v Pressure 199 80319 39823 39823 v CourantNb 1.8375 19.969 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.131000000E+02 TIME STEP NUMBER 131 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19905E+01 0.37339E+01 Friction velocity uk : 0.19905E+01 0.37339E+01 Dimensionless distance yplus : 0.49762E-01 0.93347E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62384E+01 250 0.11163E-02 0.21423E-08 0.20183E-03 c Velocity[X] 0.10213E-08 c Velocity[Y] 0.11211E-08 c Velocity[Z] 0.28258E-37 c Pressure 0.72617E-03 9 0.76212E-08 0.60278E-03 0.39734E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099067 1.0007 0.66383 0.66383 v Velocity[Y] -0.064156 0.064156 2.4332e-10 2.4332e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.4556e-21 5.4556e-21 v ǁVelocityǁ 0.099067 1.0007 0.66388 0.66388 v Pressure 199 80321 39823 39823 v CourantNb 1.8371 19.969 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.132000000E+02 TIME STEP NUMBER 132 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666986E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19906E+01 0.37338E+01 Friction velocity uk : 0.19906E+01 0.37338E+01 Dimensionless distance yplus : 0.49766E-01 0.93345E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 248 0.10833E-02 0.20131E-08 0.19565E-03 c Velocity[X] 0.95805E-09 c Velocity[Y] 0.10550E-08 c Velocity[Z] 0.25679E-37 c Pressure 0.70465E-03 9 0.73034E-08 0.58466E-03 0.37705E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099082 1.0007 0.66383 0.66383 v Velocity[Y] -0.064097 0.064097 1.9822e-10 1.9822e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.3534e-21 5.3534e-21 v ǁVelocityǁ 0.099082 1.0007 0.66388 0.66388 v Pressure 199 80323 39823 39823 v CourantNb 1.8367 19.969 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.133000000E+02 TIME STEP NUMBER 133 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19908E+01 0.37337E+01 Friction velocity uk : 0.19908E+01 0.37337E+01 Dimensionless distance yplus : 0.49770E-01 0.93343E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 246 0.10513E-02 0.18917E-08 0.18966E-03 c Velocity[X] 0.89887E-09 c Velocity[Y] 0.99287E-09 c Velocity[Z] 0.87595E-38 c Pressure 0.68377E-03 9 0.69993E-08 0.56709E-03 0.35816E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099096 1.0008 0.66383 0.66383 v Velocity[Y] -0.064039 0.064039 1.5742e-10 1.5742e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.5806e-21 4.5806e-21 v ǁVelocityǁ 0.099096 1.0008 0.66388 0.66388 v Pressure 199 80324 39823 39823 v CourantNb 1.8363 19.97 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.134000000E+02 TIME STEP NUMBER 134 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19909E+01 0.37336E+01 Friction velocity uk : 0.19909E+01 0.37336E+01 Dimensionless distance yplus : 0.49774E-01 0.93341E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 244 0.10203E-02 0.17778E-08 0.18386E-03 c Velocity[X] 0.84347E-09 c Velocity[Y] 0.93434E-09 c Velocity[Z] 0.13313E-37 c Pressure 0.66351E-03 9 0.67078E-08 0.55006E-03 0.34056E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099111 1.0008 0.66383 0.66383 v Velocity[Y] -0.063983 0.063983 1.2011e-10 1.2011e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.0662e-21 4.0662e-21 v ǁVelocityǁ 0.099111 1.0008 0.66388 0.66388 v Pressure 199 80326 39823 39823 v CourantNb 1.8357 19.97 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.135000000E+02 TIME STEP NUMBER 135 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666988E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19911E+01 0.37336E+01 Friction velocity uk : 0.19911E+01 0.37336E+01 Dimensionless distance yplus : 0.49777E-01 0.93339E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 242 0.99015E-03 0.16708E-08 0.17824E-03 c Velocity[X] 0.79158E-09 c Velocity[Y] 0.87925E-09 c Velocity[Z] 0.15762E-37 c Pressure 0.64385E-03 9 0.62015E-08 0.53354E-03 0.32413E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099125 1.0008 0.66383 0.66383 v Velocity[Y] -0.063929 0.063929 -5.9132e-11 -5.9132e-11 v Velocity[Z] -1.4597e-17 1.225e-17 3.7507e-21 3.7507e-21 v ǁVelocityǁ 0.099125 1.0008 0.66388 0.66388 v Pressure 199 80327 39823 39823 v CourantNb 1.835 19.97 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.136000000E+02 TIME STEP NUMBER 136 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19912E+01 0.37335E+01 Friction velocity uk : 0.19912E+01 0.37335E+01 Dimensionless distance yplus : 0.49781E-01 0.93337E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 240 0.96092E-03 0.15703E-08 0.17280E-03 c Velocity[X] 0.74297E-09 c Velocity[Y] 0.82738E-09 c Velocity[Z] 0.16198E-37 c Pressure 0.62476E-03 9 0.59216E-08 0.51753E-03 0.30879E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099138 1.0008 0.66383 0.66383 v Velocity[Y] -0.063876 0.063877 -9.1455e-11 -9.1455e-11 v Velocity[Z] -1.4481e-17 1.2157e-17 3.7717e-21 3.7717e-21 v ǁVelocityǁ 0.099138 1.0008 0.66388 0.66388 v Pressure 199 80328 39823 39823 v CourantNb 1.8344 19.971 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.137000000E+02 TIME STEP NUMBER 137 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19914E+01 0.37334E+01 Friction velocity uk : 0.19914E+01 0.37334E+01 Dimensionless distance yplus : 0.49784E-01 0.93335E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 238 0.93254E-03 0.14760E-08 0.16753E-03 c Velocity[X] 0.69742E-09 c Velocity[Y] 0.77855E-09 c Velocity[Z] 0.16187E-37 c Pressure 0.60624E-03 9 0.57891E-08 0.50199E-03 0.29445E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099152 1.0008 0.66383 0.66383 v Velocity[Y] -0.063826 0.063826 -1.1811e-10 -1.1811e-10 v Velocity[Z] -1.4479e-17 1.225e-17 5.0513e-21 5.0513e-21 v ǁVelocityǁ 0.099152 1.0008 0.66388 0.66388 v Pressure 199 80330 39823 39823 v CourantNb 1.8338 19.971 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.138000000E+02 TIME STEP NUMBER 138 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19915E+01 0.37333E+01 Friction velocity uk : 0.19915E+01 0.37333E+01 Dimensionless distance yplus : 0.49787E-01 0.93333E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 236 0.90500E-03 0.13873E-08 0.16242E-03 c Velocity[X] 0.65474E-09 c Velocity[Y] 0.73259E-09 c Velocity[Z] 0.18160E-37 c Pressure 0.58827E-03 9 0.55253E-08 0.48693E-03 0.28103E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099165 1.0008 0.66383 0.66383 v Velocity[Y] -0.063776 0.063776 -1.4173e-10 -1.4173e-10 v Velocity[Z] -1.4478e-17 1.225e-17 2.7282e-21 2.7282e-21 v ǁVelocityǁ 0.099165 1.0008 0.66388 0.66388 v Pressure 199 80331 39824 39824 v CourantNb 1.8332 19.971 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.139000000E+02 TIME STEP NUMBER 139 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19916E+01 0.37333E+01 Friction velocity uk : 0.19916E+01 0.37333E+01 Dimensionless distance yplus : 0.49791E-01 0.93332E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 234 0.87828E-03 0.13041E-08 0.15747E-03 c Velocity[X] 0.61473E-09 c Velocity[Y] 0.68933E-09 c Velocity[Z] 0.16103E-37 c Pressure 0.57083E-03 9 0.52986E-08 0.47233E-03 0.26845E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099178 1.0008 0.66383 0.66383 v Velocity[Y] -0.063728 0.063728 -1.5321e-10 -1.5321e-10 v Velocity[Z] -1.4596e-17 1.225e-17 4.7648e-21 4.7648e-21 v ǁVelocityǁ 0.099178 1.0008 0.66388 0.66388 v Pressure 199 80332 39824 39824 v CourantNb 1.8327 19.971 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.140000000E+02 TIME STEP NUMBER 140 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19918E+01 0.37332E+01 Friction velocity uk : 0.19918E+01 0.37332E+01 Dimensionless distance yplus : 0.49794E-01 0.93330E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 232 0.85233E-03 0.12258E-08 0.15267E-03 c Velocity[X] 0.57723E-09 c Velocity[Y] 0.64861E-09 c Velocity[Z] 0.27542E-37 c Pressure 0.55390E-03 9 0.50876E-08 0.45817E-03 0.25665E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099191 1.0008 0.66383 0.66383 v Velocity[Y] -0.063682 0.063682 -1.5982e-10 -1.5982e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.7702e-21 4.7702e-21 v ǁVelocityǁ 0.099191 1.0008 0.66388 0.66388 v Pressure 199 80333 39824 39824 v CourantNb 1.8322 19.972 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.141000000E+02 TIME STEP NUMBER 141 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19919E+01 0.37331E+01 Friction velocity uk : 0.19919E+01 0.37331E+01 Dimensionless distance yplus : 0.49797E-01 0.93328E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 230 0.82716E-03 0.11523E-08 0.14803E-03 c Velocity[X] 0.54206E-09 c Velocity[Y] 0.61028E-09 c Velocity[Z] 0.31232E-37 c Pressure 0.53748E-03 9 0.49223E-08 0.44443E-03 0.24557E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099203 1.0008 0.66383 0.66383 v Velocity[Y] -0.063637 0.063637 -1.4865e-10 -1.4865e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9115e-21 4.9115e-21 v ǁVelocityǁ 0.099203 1.0008 0.66388 0.66388 v Pressure 199 80334 39824 39824 v CourantNb 1.8316 19.972 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.142000000E+02 TIME STEP NUMBER 142 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19920E+01 0.37331E+01 Friction velocity uk : 0.19920E+01 0.37331E+01 Dimensionless distance yplus : 0.49800E-01 0.93327E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62385E+01 228 0.80273E-03 0.10833E-08 0.14352E-03 c Velocity[X] 0.50908E-09 c Velocity[Y] 0.57421E-09 c Velocity[Z] 0.14277E-37 c Pressure 0.52154E-03 9 0.47462E-08 0.43111E-03 0.23514E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099215 1.0008 0.66382 0.66382 v Velocity[Y] -0.063593 0.063593 -1.4339e-10 -1.4339e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.6534e-21 4.6534e-21 v ǁVelocityǁ 0.099215 1.0008 0.66388 0.66388 v Pressure 199 80335 39824 39824 v CourantNb 1.8311 19.972 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.143000000E+02 TIME STEP NUMBER 143 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19921E+01 0.37330E+01 Friction velocity uk : 0.19921E+01 0.37330E+01 Dimensionless distance yplus : 0.49803E-01 0.93325E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 226 0.77902E-03 0.10184E-08 0.13916E-03 c Velocity[X] 0.47815E-09 c Velocity[Y] 0.54027E-09 c Velocity[Z] 0.18071E-37 c Pressure 0.50607E-03 10 0.98133E-08 0.41819E-03 0.22532E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099226 1.0008 0.66382 0.66382 v Velocity[Y] -0.063551 0.063551 -2.4528e-09 -2.4528e-09 v Velocity[Z] -1.4597e-17 1.225e-17 3.2514e-21 3.2514e-21 v ǁVelocityǁ 0.099226 1.0008 0.66388 0.66388 v Pressure 199 80336 39824 39824 v CourantNb 1.8307 19.972 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.144000000E+02 TIME STEP NUMBER 144 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666975E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19922E+01 0.37330E+01 Friction velocity uk : 0.19922E+01 0.37330E+01 Dimensionless distance yplus : 0.49806E-01 0.93324E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 224 0.75601E-03 0.95744E-09 0.13493E-03 c Velocity[X] 0.44914E-09 c Velocity[Y] 0.50831E-09 c Velocity[Z] 0.15049E-37 c Pressure 0.49106E-03 10 0.93387E-08 0.40567E-03 0.21607E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099236 1.0008 0.66382 0.66382 v Velocity[Y] -0.06351 0.06351 -2.3357e-09 -2.3357e-09 v Velocity[Z] -1.4479e-17 1.2195e-17 6.2892e-21 6.2892e-21 v ǁVelocityǁ 0.099236 1.0008 0.66388 0.66388 v Pressure 199 80337 39824 39824 v CourantNb 1.8302 19.972 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.145000000E+02 TIME STEP NUMBER 145 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666980E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19923E+01 0.37329E+01 Friction velocity uk : 0.19923E+01 0.37329E+01 Dimensionless distance yplus : 0.49809E-01 0.93322E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 222 0.73368E-03 0.90012E-09 0.13083E-03 c Velocity[X] 0.42189E-09 c Velocity[Y] 0.47822E-09 c Velocity[Z] 0.25565E-37 c Pressure 0.47649E-03 9 0.96210E-08 0.39352E-03 0.20733E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099245 1.0008 0.66382 0.66382 v Velocity[Y] -0.06347 0.06347 -2.5341e-09 -2.5341e-09 v Velocity[Z] -1.4475e-17 1.2192e-17 2.9807e-21 2.9807e-21 v ǁVelocityǁ 0.099245 1.0008 0.66387 0.66387 v Pressure 199 80338 39824 39824 v CourantNb 1.8298 19.973 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.146000000E+02 TIME STEP NUMBER 146 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666979E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19924E+01 0.37328E+01 Friction velocity uk : 0.19924E+01 0.37328E+01 Dimensionless distance yplus : 0.49811E-01 0.93321E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 221 0.71200E-03 0.84632E-09 0.12686E-03 c Velocity[X] 0.39637E-09 c Velocity[Y] 0.44995E-09 c Velocity[Z] 0.23929E-37 c Pressure 0.46235E-03 9 0.91200E-08 0.38173E-03 0.19907E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099255 1.0008 0.66382 0.66382 v Velocity[Y] -0.063431 0.063431 -2.4233e-09 -2.4233e-09 v Velocity[Z] -1.4483e-17 1.2168e-17 4.7809e-21 4.7809e-21 v ǁVelocityǁ 0.099255 1.0008 0.66387 0.66387 v Pressure 199 80339 39824 39824 v CourantNb 1.8293 19.973 13.417 13.417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.147000000E+02 TIME STEP NUMBER 147 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666980E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19925E+01 0.37328E+01 Friction velocity uk : 0.19925E+01 0.37328E+01 Dimensionless distance yplus : 0.49813E-01 0.93320E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 219 0.69097E-03 0.79572E-09 0.12301E-03 c Velocity[X] 0.37241E-09 c Velocity[Y] 0.42331E-09 c Velocity[Z] 0.21227E-37 c Pressure 0.44864E-03 9 0.86507E-08 0.37030E-03 0.19125E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099264 1.0008 0.66382 0.66382 v Velocity[Y] -0.063394 0.063394 -2.3224e-09 -2.3224e-09 v Velocity[Z] -1.4597e-17 1.2253e-17 4.4942e-21 4.4942e-21 v ǁVelocityǁ 0.099264 1.0008 0.66387 0.66387 v Pressure 199 80340 39824 39824 v CourantNb 1.8289 19.973 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.148000000E+02 TIME STEP NUMBER 148 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666981E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19926E+01 0.37327E+01 Friction velocity uk : 0.19926E+01 0.37327E+01 Dimensionless distance yplus : 0.49816E-01 0.93318E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 217 0.67055E-03 0.74817E-09 0.11927E-03 c Velocity[X] 0.34991E-09 c Velocity[Y] 0.39826E-09 c Velocity[Z] 0.17937E-37 c Pressure 0.43532E-03 9 0.82035E-08 0.35922E-03 0.18385E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099273 1.0008 0.66382 0.66382 v Velocity[Y] -0.063358 0.063358 -2.2245e-09 -2.2245e-09 v Velocity[Z] -1.4597e-17 1.225e-17 3.9599e-21 3.9599e-21 v ǁVelocityǁ 0.099273 1.0008 0.66387 0.66387 v Pressure 199 80341 39824 39824 v CourantNb 1.8285 19.973 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.149000000E+02 TIME STEP NUMBER 149 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19927E+01 0.37327E+01 Friction velocity uk : 0.19927E+01 0.37327E+01 Dimensionless distance yplus : 0.49818E-01 0.93317E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 216 0.65074E-03 0.70347E-09 0.11566E-03 c Velocity[X] 0.32879E-09 c Velocity[Y] 0.37468E-09 c Velocity[Z] 0.24778E-37 c Pressure 0.42241E-03 9 0.77785E-08 0.34847E-03 0.17683E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099282 1.0008 0.66382 0.66382 v Velocity[Y] -0.063322 0.063322 -2.129e-09 -2.129e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.9962e-21 6.9962e-21 v ǁVelocityǁ 0.099282 1.0008 0.66387 0.66387 v Pressure 199 80342 39824 39824 v CourantNb 1.8281 19.973 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.150000000E+02 TIME STEP NUMBER 150 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19928E+01 0.37326E+01 Friction velocity uk : 0.19928E+01 0.37326E+01 Dimensionless distance yplus : 0.49820E-01 0.93316E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 214 0.63151E-03 0.66146E-09 0.11215E-03 c Velocity[X] 0.30897E-09 c Velocity[Y] 0.35249E-09 c Velocity[Z] 0.21426E-37 c Pressure 0.40987E-03 9 0.73751E-08 0.33804E-03 0.17016E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099291 1.0008 0.66382 0.66382 v Velocity[Y] -0.063288 0.063288 -2.0359e-09 -2.0359e-09 v Velocity[Z] -1.4597e-17 1.225e-17 3.8417e-21 3.8417e-21 v ǁVelocityǁ 0.099291 1.0008 0.66387 0.66387 v Pressure 199 80343 39824 39824 v CourantNb 1.8278 19.973 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.151000000E+02 TIME STEP NUMBER 151 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19929E+01 0.37326E+01 Friction velocity uk : 0.19929E+01 0.37326E+01 Dimensionless distance yplus : 0.49822E-01 0.93315E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 212 0.61285E-03 0.62197E-09 0.10875E-03 c Velocity[X] 0.29037E-09 c Velocity[Y] 0.33161E-09 c Velocity[Z] 0.10091E-37 c Pressure 0.39770E-03 9 0.69927E-08 0.32793E-03 0.16381E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099299 1.0008 0.66382 0.66382 v Velocity[Y] -0.063255 0.063255 -1.9448e-09 -1.9448e-09 v Velocity[Z] -1.4597e-17 1.225e-17 3.0608e-21 3.0608e-21 v ǁVelocityǁ 0.099299 1.0008 0.66387 0.66387 v Pressure 199 80343 39824 39824 v CourantNb 1.8274 19.974 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.152000000E+02 TIME STEP NUMBER 152 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19930E+01 0.37325E+01 Friction velocity uk : 0.19930E+01 0.37325E+01 Dimensionless distance yplus : 0.49824E-01 0.93314E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 211 0.59474E-03 0.58486E-09 0.10546E-03 c Velocity[X] 0.27289E-09 c Velocity[Y] 0.31198E-09 c Velocity[Z] 0.15589E-37 c Pressure 0.38590E-03 8 0.99850E-08 0.31812E-03 0.15778E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099307 1.0008 0.66382 0.66382 v Velocity[Y] -0.063223 0.063223 -2.0571e-09 -2.0571e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.6879e-21 5.6879e-21 v ǁVelocityǁ 0.099308 1.0008 0.66387 0.66387 v Pressure 199 80344 39824 39824 v CourantNb 1.8271 19.974 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.153000000E+02 TIME STEP NUMBER 153 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19931E+01 0.37325E+01 Friction velocity uk : 0.19931E+01 0.37325E+01 Dimensionless distance yplus : 0.49827E-01 0.93313E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 209 0.57716E-03 0.54996E-09 0.10226E-03 c Velocity[X] 0.25649E-09 c Velocity[Y] 0.29347E-09 c Velocity[Z] 0.14151E-37 c Pressure 0.37444E-03 8 0.94477E-08 0.30860E-03 0.15203E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099315 1.0008 0.66382 0.66382 v Velocity[Y] -0.063192 0.063192 -1.9585e-09 -1.9585e-09 v Velocity[Z] -1.4477e-17 1.2195e-17 5.3618e-21 5.3618e-21 v ǁVelocityǁ 0.099316 1.0008 0.66387 0.66387 v Pressure 199 80345 39824 39824 v CourantNb 1.8268 19.974 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.154000000E+02 TIME STEP NUMBER 154 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19931E+01 0.37325E+01 Friction velocity uk : 0.19931E+01 0.37325E+01 Dimensionless distance yplus : 0.49829E-01 0.93312E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 208 0.56010E-03 0.51716E-09 0.99166E-04 c Velocity[X] 0.24107E-09 c Velocity[Y] 0.27608E-09 c Velocity[Z] 0.22507E-37 c Pressure 0.36333E-03 8 0.89534E-08 0.29937E-03 0.14654E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099323 1.0008 0.66382 0.66382 v Velocity[Y] -0.063162 0.063162 -1.8625e-09 -1.8625e-09 v Velocity[Z] -1.4596e-17 1.225e-17 6.0357e-21 6.0357e-21 v ǁVelocityǁ 0.099323 1.0008 0.66387 0.66387 v Pressure 199 80346 39824 39824 v CourantNb 1.8264 19.974 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.155000000E+02 TIME STEP NUMBER 155 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666986E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19932E+01 0.37324E+01 Friction velocity uk : 0.19932E+01 0.37324E+01 Dimensionless distance yplus : 0.49831E-01 0.93310E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 206 0.54355E-03 0.48633E-09 0.96164E-04 c Velocity[X] 0.22661E-09 c Velocity[Y] 0.25972E-09 c Velocity[Z] 0.13316E-37 c Pressure 0.35254E-03 8 0.84975E-08 0.29042E-03 0.14131E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099331 1.0008 0.66382 0.66382 v Velocity[Y] -0.063133 0.063133 -1.7698e-09 -1.7698e-09 v Velocity[Z] -1.4597e-17 1.225e-17 4.1531e-21 4.1531e-21 v ǁVelocityǁ 0.099331 1.0008 0.66387 0.66387 v Pressure 199 80346 39824 39824 v CourantNb 1.8261 19.974 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.156000000E+02 TIME STEP NUMBER 156 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666986E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19933E+01 0.37324E+01 Friction velocity uk : 0.19933E+01 0.37324E+01 Dimensionless distance yplus : 0.49832E-01 0.93309E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 205 0.52748E-03 0.45734E-09 0.93254E-04 c Velocity[X] 0.21302E-09 c Velocity[Y] 0.24432E-09 c Velocity[Z] 0.13220E-37 c Pressure 0.34207E-03 8 0.80735E-08 0.28174E-03 0.13631E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099337 1.0008 0.66382 0.66382 v Velocity[Y] -0.063104 0.063104 -1.68e-09 -1.68e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.0711e-21 6.0711e-21 v ǁVelocityǁ 0.099337 1.0008 0.66387 0.66387 v Pressure 199 80347 39824 39824 v CourantNb 1.8258 19.974 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.157000000E+02 TIME STEP NUMBER 157 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19934E+01 0.37323E+01 Friction velocity uk : 0.19934E+01 0.37323E+01 Dimensionless distance yplus : 0.49834E-01 0.93309E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 203 0.51189E-03 0.43009E-09 0.90433E-04 c Velocity[X] 0.20025E-09 c Velocity[Y] 0.22983E-09 c Velocity[Z] 0.22675E-37 c Pressure 0.33191E-03 8 0.76735E-08 0.27332E-03 0.13153E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099343 1.0008 0.66382 0.66382 v Velocity[Y] -0.063077 0.063077 -1.5935e-09 -1.5935e-09 v Velocity[Z] -1.4597e-17 1.2251e-17 6.6902e-21 6.6902e-21 v ǁVelocityǁ 0.099343 1.0008 0.66387 0.66387 v Pressure 199 80348 39824 39824 v CourantNb 1.8255 19.974 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.158000000E+02 TIME STEP NUMBER 158 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19934E+01 0.37323E+01 Friction velocity uk : 0.19934E+01 0.37323E+01 Dimensionless distance yplus : 0.49836E-01 0.93308E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62386E+01 202 0.49676E-03 0.40446E-09 0.87698E-04 c Velocity[X] 0.18825E-09 c Velocity[Y] 0.21621E-09 c Velocity[Z] 0.12903E-37 c Pressure 0.32205E-03 8 0.72245E-08 0.26515E-03 0.12695E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099349 1.0008 0.66382 0.66382 v Velocity[Y] -0.06305 0.06305 -1.5163e-09 -1.5163e-09 v Velocity[Z] -1.4597e-17 1.2251e-17 5.163e-21 5.163e-21 v ǁVelocityǁ 0.099349 1.0008 0.66387 0.66387 v Pressure 199 80348 39824 39824 v CourantNb 1.8253 19.974 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.159000000E+02 TIME STEP NUMBER 159 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19935E+01 0.37323E+01 Friction velocity uk : 0.19935E+01 0.37323E+01 Dimensionless distance yplus : 0.49837E-01 0.93307E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 200 0.48207E-03 0.38037E-09 0.85046E-04 c Velocity[X] 0.17699E-09 c Velocity[Y] 0.20338E-09 c Velocity[Z] 0.18512E-37 c Pressure 0.31249E-03 8 0.62149E-08 0.25722E-03 0.12255E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099354 1.0008 0.66382 0.66382 v Velocity[Y] -0.063024 0.063024 -1.2316e-09 -1.2316e-09 v Velocity[Z] -1.4597e-17 1.225e-17 3.0979e-21 3.0979e-21 v ǁVelocityǁ 0.099354 1.0008 0.66387 0.66387 v Pressure 199 80349 39824 39824 v CourantNb 1.825 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.160000000E+02 TIME STEP NUMBER 160 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19935E+01 0.37322E+01 Friction velocity uk : 0.19935E+01 0.37322E+01 Dimensionless distance yplus : 0.49838E-01 0.93306E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 199 0.46782E-03 0.35772E-09 0.82475E-04 c Velocity[X] 0.16640E-09 c Velocity[Y] 0.19132E-09 c Velocity[Z] 0.18126E-37 c Pressure 0.30321E-03 8 0.56290E-08 0.24954E-03 0.11834E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09936 1.0008 0.66382 0.66382 v Velocity[Y] -0.062999 0.062999 -1.0119e-09 -1.0119e-09 v Velocity[Z] -1.4481e-17 1.2157e-17 5.8178e-21 5.8178e-21 v ǁVelocityǁ 0.09936 1.0008 0.66387 0.66387 v Pressure 199 80349 39824 39824 v CourantNb 1.8247 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.161000000E+02 TIME STEP NUMBER 161 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19936E+01 0.37322E+01 Friction velocity uk : 0.19936E+01 0.37322E+01 Dimensionless distance yplus : 0.49840E-01 0.93305E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 198 0.45399E-03 0.33643E-09 0.79982E-04 c Velocity[X] 0.15646E-09 c Velocity[Y] 0.17997E-09 c Velocity[Z] 0.19907E-37 c Pressure 0.29420E-03 8 0.53394E-08 0.24208E-03 0.11432E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099365 1.0008 0.66382 0.66382 v Velocity[Y] -0.062975 0.062975 -9.3039e-10 -9.3039e-10 v Velocity[Z] -1.4474e-17 1.2164e-17 2.7447e-21 2.7447e-21 v ǁVelocityǁ 0.099365 1.0008 0.66387 0.66387 v Pressure 199 80350 39824 39824 v CourantNb 1.8245 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.162000000E+02 TIME STEP NUMBER 162 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19936E+01 0.37322E+01 Friction velocity uk : 0.19936E+01 0.37322E+01 Dimensionless distance yplus : 0.49841E-01 0.93304E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 196 0.44056E-03 0.31640E-09 0.77566E-04 c Velocity[X] 0.14712E-09 c Velocity[Y] 0.16929E-09 c Velocity[Z] 0.25721E-37 c Pressure 0.28546E-03 8 0.50682E-08 0.23485E-03 0.11045E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09937 1.0008 0.66382 0.66382 v Velocity[Y] -0.062951 0.062951 -8.8104e-10 -8.8104e-10 v Velocity[Z] -1.4476e-17 1.2184e-17 6.0309e-21 6.0309e-21 v ǁVelocityǁ 0.09937 1.0008 0.66387 0.66387 v Pressure 199 80351 39824 39824 v CourantNb 1.8243 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.163000000E+02 TIME STEP NUMBER 163 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666988E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19937E+01 0.37321E+01 Friction velocity uk : 0.19937E+01 0.37321E+01 Dimensionless distance yplus : 0.49842E-01 0.93303E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 195 0.42753E-03 0.29758E-09 0.75223E-04 c Velocity[X] 0.13833E-09 c Velocity[Y] 0.15924E-09 c Velocity[Z] 0.14992E-37 c Pressure 0.27698E-03 8 0.48142E-08 0.22783E-03 0.10674E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099375 1.0008 0.66382 0.66382 v Velocity[Y] -0.062929 0.062929 -8.3398e-10 -8.3398e-10 v Velocity[Z] -1.4596e-17 1.2229e-17 6.0901e-21 6.0901e-21 v ǁVelocityǁ 0.099375 1.0008 0.66387 0.66387 v Pressure 199 80351 39824 39824 v CourantNb 1.824 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.164000000E+02 TIME STEP NUMBER 164 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19937E+01 0.37321E+01 Friction velocity uk : 0.19937E+01 0.37321E+01 Dimensionless distance yplus : 0.49844E-01 0.93302E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 194 0.41489E-03 0.27987E-09 0.72951E-04 c Velocity[X] 0.13008E-09 c Velocity[Y] 0.14979E-09 c Velocity[Z] 0.23823E-37 c Pressure 0.26875E-03 8 0.47029E-08 0.22103E-03 0.10317E-04 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09938 1.0008 0.66382 0.66382 v Velocity[Y] -0.062906 0.062906 -7.8205e-10 -7.8205e-10 v Velocity[Z] -1.4597e-17 1.2157e-17 3.1888e-21 3.1888e-21 v ǁVelocityǁ 0.09938 1.0008 0.66387 0.66387 v Pressure 199 80352 39824 39824 v CourantNb 1.8238 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.165000000E+02 TIME STEP NUMBER 165 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19938E+01 0.37321E+01 Friction velocity uk : 0.19938E+01 0.37321E+01 Dimensionless distance yplus : 0.49845E-01 0.93302E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 192 0.40262E-03 0.26323E-09 0.70748E-04 c Velocity[X] 0.12233E-09 c Velocity[Y] 0.14090E-09 c Velocity[Z] 0.32126E-37 c Pressure 0.26076E-03 8 0.44794E-08 0.21443E-03 0.99743E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099385 1.0008 0.66382 0.66382 v Velocity[Y] -0.062885 0.062885 -7.3962e-10 -7.3962e-10 v Velocity[Z] -1.4475e-17 1.225e-17 3.5511e-21 3.5511e-21 v ǁVelocityǁ 0.099385 1.0008 0.66387 0.66387 v Pressure 199 80352 39824 39824 v CourantNb 1.8236 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.166000000E+02 TIME STEP NUMBER 166 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666988E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19938E+01 0.37320E+01 Friction velocity uk : 0.19938E+01 0.37320E+01 Dimensionless distance yplus : 0.49846E-01 0.93301E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 191 0.39071E-03 0.24757E-09 0.68612E-04 c Velocity[X] 0.11503E-09 c Velocity[Y] 0.13254E-09 c Velocity[Z] 0.17483E-37 c Pressure 0.25301E-03 7 0.98321E-08 0.20802E-03 0.96444E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099389 1.0009 0.66382 0.66382 v Velocity[Y] -0.062864 0.062864 -7.5571e-10 -7.5571e-10 v Velocity[Z] -1.4596e-17 1.225e-17 2.7288e-21 2.7288e-21 v ǁVelocityǁ 0.099389 1.0009 0.66387 0.66387 v Pressure 199 80353 39824 39824 v CourantNb 1.8234 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.167000000E+02 TIME STEP NUMBER 167 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19939E+01 0.37320E+01 Friction velocity uk : 0.19939E+01 0.37320E+01 Dimensionless distance yplus : 0.49847E-01 0.93300E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 190 0.37915E-03 0.23285E-09 0.66541E-04 c Velocity[X] 0.10818E-09 c Velocity[Y] 0.12467E-09 c Velocity[Z] 0.22848E-37 c Pressure 0.24549E-03 7 0.94007E-08 0.20181E-03 0.93269E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099394 1.0009 0.66382 0.66382 v Velocity[Y] -0.062844 0.062844 -7.1471e-10 -7.1471e-10 v Velocity[Z] -1.4481e-17 1.2186e-17 5.4936e-21 5.4936e-21 v ǁVelocityǁ 0.099394 1.0009 0.66387 0.66387 v Pressure 199 80353 39824 39824 v CourantNb 1.8232 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.168000000E+02 TIME STEP NUMBER 168 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19939E+01 0.37320E+01 Friction velocity uk : 0.19939E+01 0.37320E+01 Dimensionless distance yplus : 0.49848E-01 0.93300E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 189 0.36794E-03 0.21901E-09 0.64533E-04 c Velocity[X] 0.10174E-09 c Velocity[Y] 0.11727E-09 c Velocity[Z] 0.12849E-37 c Pressure 0.23820E-03 7 0.89932E-08 0.19578E-03 0.90211E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099397 1.0009 0.66382 0.66382 v Velocity[Y] -0.062824 0.062824 -6.754e-10 -6.754e-10 v Velocity[Z] -1.4485e-17 1.2252e-17 7.5646e-21 7.5646e-21 v ǁVelocityǁ 0.099397 1.0009 0.66387 0.66387 v Pressure 199 80353 39824 39824 v CourantNb 1.823 19.975 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.169000000E+02 TIME STEP NUMBER 169 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19940E+01 0.37320E+01 Friction velocity uk : 0.19940E+01 0.37320E+01 Dimensionless distance yplus : 0.49849E-01 0.93299E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 187 0.35705E-03 0.20600E-09 0.62586E-04 c Velocity[X] 0.95690E-10 c Velocity[Y] 0.11031E-09 c Velocity[Z] 0.14291E-37 c Pressure 0.23112E-03 7 0.86074E-08 0.18994E-03 0.87265E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.0994 1.0009 0.66382 0.66382 v Velocity[Y] -0.062806 0.062806 -6.378e-10 -6.378e-10 v Velocity[Z] -1.4596e-17 1.2251e-17 5.8122e-21 5.8122e-21 v ǁVelocityǁ 0.0994 1.0009 0.66387 0.66387 v Pressure 199 80354 39824 39824 v CourantNb 1.8228 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.170000000E+02 TIME STEP NUMBER 170 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19940E+01 0.37319E+01 Friction velocity uk : 0.19940E+01 0.37319E+01 Dimensionless distance yplus : 0.49850E-01 0.93298E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 186 0.34649E-03 0.19375E-09 0.60698E-04 c Velocity[X] 0.89995E-10 c Velocity[Y] 0.10376E-09 c Velocity[Z] 0.16903E-37 c Pressure 0.22425E-03 7 0.82427E-08 0.18427E-03 0.84427E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099403 1.0009 0.66382 0.66382 v Velocity[Y] -0.062787 0.062787 -6.0221e-10 -6.0221e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.1596e-21 7.1596e-21 v ǁVelocityǁ 0.099403 1.0009 0.66387 0.66387 v Pressure 199 80354 39824 39824 v CourantNb 1.8226 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.171000000E+02 TIME STEP NUMBER 171 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19940E+01 0.37319E+01 Friction velocity uk : 0.19940E+01 0.37319E+01 Dimensionless distance yplus : 0.49851E-01 0.93298E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 185 0.33624E-03 0.18226E-09 0.58870E-04 c Velocity[X] 0.84663E-10 c Velocity[Y] 0.97597E-10 c Velocity[Z] 0.27540E-37 c Pressure 0.21758E-03 8 0.96495E-08 0.17876E-03 0.81690E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099406 1.0009 0.66382 0.66382 v Velocity[Y] -0.062769 0.062769 -9.8552e-10 -9.8552e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5087e-21 5.5087e-21 v ǁVelocityǁ 0.099406 1.0009 0.66387 0.66387 v Pressure 199 80355 39824 39824 v CourantNb 1.8225 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.172000000E+02 TIME STEP NUMBER 172 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19941E+01 0.37319E+01 Friction velocity uk : 0.19941E+01 0.37319E+01 Dimensionless distance yplus : 0.49851E-01 0.93297E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 184 0.32629E-03 0.17141E-09 0.57092E-04 c Velocity[X] 0.79614E-10 c Velocity[Y] 0.91800E-10 c Velocity[Z] 0.35546E-37 c Pressure 0.21111E-03 8 0.92688E-08 0.17343E-03 0.79052E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099409 1.0009 0.66382 0.66382 v Velocity[Y] -0.062752 0.062752 -9.0858e-10 -9.0858e-10 v Velocity[Z] -1.4482e-17 1.2159e-17 9.4482e-21 9.4482e-21 v ǁVelocityǁ 0.099409 1.0009 0.66387 0.66387 v Pressure 199 80355 39824 39824 v CourantNb 1.8223 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.173000000E+02 TIME STEP NUMBER 173 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19941E+01 0.37319E+01 Friction velocity uk : 0.19941E+01 0.37319E+01 Dimensionless distance yplus : 0.49852E-01 0.93296E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 182 0.31664E-03 0.16124E-09 0.55371E-04 c Velocity[X] 0.74889E-10 c Velocity[Y] 0.86346E-10 c Velocity[Z] 0.24531E-37 c Pressure 0.20484E-03 8 0.89058E-08 0.16825E-03 0.76506E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099412 1.0009 0.66382 0.66382 v Velocity[Y] -0.062735 0.062735 -8.3484e-10 -8.3484e-10 v Velocity[Z] -1.4596e-17 1.225e-17 7.1626e-21 7.1626e-21 v ǁVelocityǁ 0.099412 1.0009 0.66387 0.66387 v Pressure 199 80355 39824 39824 v CourantNb 1.8221 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.174000000E+02 TIME STEP NUMBER 174 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19941E+01 0.37318E+01 Friction velocity uk : 0.19941E+01 0.37318E+01 Dimensionless distance yplus : 0.49853E-01 0.93296E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 181 0.30727E-03 0.15166E-09 0.53701E-04 c Velocity[X] 0.70439E-10 c Velocity[Y] 0.81220E-10 c Velocity[Z] 0.39123E-37 c Pressure 0.19875E-03 8 0.85604E-08 0.16323E-03 0.74050E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099414 1.0009 0.66382 0.66382 v Velocity[Y] -0.062719 0.062719 -7.6638e-10 -7.6638e-10 v Velocity[Z] -1.4597e-17 1.225e-17 9.1213e-22 9.1213e-22 v ǁVelocityǁ 0.099414 1.0009 0.66387 0.66387 v Pressure 199 80356 39824 39824 v CourantNb 1.822 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.175000000E+02 TIME STEP NUMBER 175 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19941E+01 0.37318E+01 Friction velocity uk : 0.19941E+01 0.37318E+01 Dimensionless distance yplus : 0.49853E-01 0.93295E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 180 0.29817E-03 0.14265E-09 0.52083E-04 c Velocity[X] 0.66258E-10 c Velocity[Y] 0.76396E-10 c Velocity[Z] 0.26958E-37 c Pressure 0.19284E-03 8 0.82311E-08 0.15836E-03 0.71680E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099417 1.0009 0.66382 0.66382 v Velocity[Y] -0.062703 0.062703 -7.027e-10 -7.027e-10 v Velocity[Z] -1.4597e-17 1.2251e-17 7.2274e-21 7.2274e-21 v ǁVelocityǁ 0.099417 1.0009 0.66387 0.66387 v Pressure 199 80356 39824 39824 v CourantNb 1.8218 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.176000000E+02 TIME STEP NUMBER 176 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19942E+01 0.37318E+01 Friction velocity uk : 0.19942E+01 0.37318E+01 Dimensionless distance yplus : 0.49854E-01 0.93295E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 179 0.28935E-03 0.13418E-09 0.50513E-04 c Velocity[X] 0.62328E-10 c Velocity[Y] 0.71857E-10 c Velocity[Z] 0.17213E-37 c Pressure 0.18710E-03 8 0.77439E-08 0.15363E-03 0.69378E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099419 1.0009 0.66382 0.66382 v Velocity[Y] -0.062688 0.062688 -2.7005e-10 -2.7005e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.6481e-21 6.6481e-21 v ǁVelocityǁ 0.09942 1.0009 0.66387 0.66387 v Pressure 199 80356 39824 39824 v CourantNb 1.8217 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.177000000E+02 TIME STEP NUMBER 177 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19942E+01 0.37318E+01 Friction velocity uk : 0.19942E+01 0.37318E+01 Dimensionless distance yplus : 0.49855E-01 0.93294E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 178 0.28079E-03 0.12622E-09 0.48991E-04 c Velocity[X] 0.58631E-10 c Velocity[Y] 0.67589E-10 c Velocity[Z] 0.34036E-37 c Pressure 0.18154E-03 8 0.74581E-08 0.14904E-03 0.67171E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099422 1.0009 0.66382 0.66382 v Velocity[Y] -0.062673 0.062673 -2.3331e-10 -2.3331e-10 v Velocity[Z] -1.4481e-17 1.2166e-17 5.5837e-21 5.5837e-21 v ǁVelocityǁ 0.099422 1.0009 0.66387 0.66387 v Pressure 199 80357 39824 39824 v CourantNb 1.8215 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.178000000E+02 TIME STEP NUMBER 178 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19942E+01 0.37317E+01 Friction velocity uk : 0.19942E+01 0.37317E+01 Dimensionless distance yplus : 0.49855E-01 0.93294E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 176 0.27248E-03 0.11873E-09 0.47515E-04 c Velocity[X] 0.55159E-10 c Velocity[Y] 0.63572E-10 c Velocity[Z] 0.27723E-37 c Pressure 0.17614E-03 8 0.71720E-08 0.14460E-03 0.65036E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099424 1.0009 0.66382 0.66382 v Velocity[Y] -0.062659 0.062659 -1.5393e-10 -1.5393e-10 v Velocity[Z] -1.4602e-17 1.2198e-17 5.6877e-21 5.6877e-21 v ǁVelocityǁ 0.099424 1.0009 0.66387 0.66387 v Pressure 199 80357 39824 39824 v CourantNb 1.8214 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.179000000E+02 TIME STEP NUMBER 179 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19942E+01 0.37317E+01 Friction velocity uk : 0.19942E+01 0.37317E+01 Dimensionless distance yplus : 0.49856E-01 0.93293E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 175 0.26441E-03 0.11168E-09 0.46083E-04 c Velocity[X] 0.51887E-10 c Velocity[Y] 0.59797E-10 c Velocity[Z] 0.27125E-37 c Pressure 0.17090E-03 8 0.69101E-08 0.14028E-03 0.62975E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099426 1.0009 0.66382 0.66382 v Velocity[Y] -0.062645 0.062645 -1.2818e-10 -1.2818e-10 v Velocity[Z] -1.4475e-17 1.2183e-17 6.1569e-21 6.1569e-21 v ǁVelocityǁ 0.099426 1.0009 0.66387 0.66387 v Pressure 199 80357 39824 39824 v CourantNb 1.8213 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.180000000E+02 TIME STEP NUMBER 180 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666988E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19943E+01 0.37317E+01 Friction velocity uk : 0.19943E+01 0.37317E+01 Dimensionless distance yplus : 0.49856E-01 0.93293E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 174 0.25658E-03 0.10506E-09 0.44695E-04 c Velocity[X] 0.48813E-10 c Velocity[Y] 0.56244E-10 c Velocity[Z] 0.25012E-37 c Pressure 0.16581E-03 8 0.66660E-08 0.13609E-03 0.60984E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099428 1.0009 0.66382 0.66382 v Velocity[Y] -0.062632 0.062632 -1.0894e-10 -1.0894e-10 v Velocity[Z] -1.4519e-17 1.2188e-17 4.415e-21 4.415e-21 v ǁVelocityǁ 0.099428 1.0009 0.66387 0.66387 v Pressure 199 80358 39824 39824 v CourantNb 1.8211 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.181000000E+02 TIME STEP NUMBER 181 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19943E+01 0.37317E+01 Friction velocity uk : 0.19943E+01 0.37317E+01 Dimensionless distance yplus : 0.49857E-01 0.93292E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 173 0.24899E-03 0.98825E-10 0.43349E-04 c Velocity[X] 0.45922E-10 c Velocity[Y] 0.52903E-10 c Velocity[Z] 0.10678E-37 c Pressure 0.16088E-03 8 0.64218E-08 0.13203E-03 0.59059E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099429 1.0009 0.66382 0.66382 v Velocity[Y] -0.062618 0.062618 -8.328e-11 -8.328e-11 v Velocity[Z] -1.4518e-17 1.2187e-17 5.338e-21 5.338e-21 v ǁVelocityǁ 0.099429 1.0009 0.66387 0.66387 v Pressure 199 80358 39824 39824 v CourantNb 1.821 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.182000000E+02 TIME STEP NUMBER 182 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19943E+01 0.37317E+01 Friction velocity uk : 0.19943E+01 0.37317E+01 Dimensionless distance yplus : 0.49857E-01 0.93292E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 172 0.24162E-03 0.92963E-10 0.42044E-04 c Velocity[X] 0.43204E-10 c Velocity[Y] 0.49759E-10 c Velocity[Z] 0.22655E-37 c Pressure 0.15610E-03 8 0.61921E-08 0.12809E-03 0.57199E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099431 1.0009 0.66382 0.66382 v Velocity[Y] -0.062606 0.062606 -6.3801e-11 -6.3801e-11 v Velocity[Z] -1.448e-17 1.219e-17 6.8399e-21 6.8399e-21 v ǁVelocityǁ 0.099431 1.0009 0.66387 0.66387 v Pressure 199 80358 39824 39824 v CourantNb 1.8209 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.183000000E+02 TIME STEP NUMBER 183 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19943E+01 0.37317E+01 Friction velocity uk : 0.19943E+01 0.37317E+01 Dimensionless distance yplus : 0.49857E-01 0.93291E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 171 0.23446E-03 0.87445E-10 0.40777E-04 c Velocity[X] 0.40648E-10 c Velocity[Y] 0.46797E-10 c Velocity[Z] 0.31080E-37 c Pressure 0.15145E-03 7 0.97530E-08 0.12427E-03 0.55399E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099432 1.0009 0.66382 0.66382 v Velocity[Y] -0.062594 0.062593 -9.6202e-11 -9.6202e-11 v Velocity[Z] -1.448e-17 1.2192e-17 5.2557e-21 5.2557e-21 v ǁVelocityǁ 0.099432 1.0009 0.66387 0.66387 v Pressure 199 80359 39824 39824 v CourantNb 1.8208 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.184000000E+02 TIME STEP NUMBER 184 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19943E+01 0.37316E+01 Friction velocity uk : 0.19943E+01 0.37316E+01 Dimensionless distance yplus : 0.49858E-01 0.93291E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 170 0.22752E-03 0.82264E-10 0.39551E-04 c Velocity[X] 0.38242E-10 c Velocity[Y] 0.44022E-10 c Velocity[Z] 0.19012E-37 c Pressure 0.14695E-03 7 0.94231E-08 0.12056E-03 0.53660E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099433 1.0009 0.66382 0.66382 v Velocity[Y] -0.062582 0.062582 -7.5396e-11 -7.5396e-11 v Velocity[Z] -1.4481e-17 1.217e-17 6.5158e-21 6.5158e-21 v ǁVelocityǁ 0.099433 1.0009 0.66387 0.66387 v Pressure 199 80359 39824 39824 v CourantNb 1.8207 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.185000000E+02 TIME STEP NUMBER 185 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19943E+01 0.37316E+01 Friction velocity uk : 0.19943E+01 0.37316E+01 Dimensionless distance yplus : 0.49858E-01 0.93291E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 169 0.22078E-03 0.77386E-10 0.38360E-04 c Velocity[X] 0.35980E-10 c Velocity[Y] 0.41406E-10 c Velocity[Z] 0.14113E-37 c Pressure 0.14257E-03 7 0.91053E-08 0.11697E-03 0.51977E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099435 1.0009 0.66381 0.66381 v Velocity[Y] -0.06257 0.06257 -5.4053e-11 -5.4053e-11 v Velocity[Z] -1.4477e-17 1.2162e-17 5.3027e-21 5.3027e-21 v ǁVelocityǁ 0.099435 1.0009 0.66387 0.66387 v Pressure 199 80359 39824 39824 v CourantNb 1.8206 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.186000000E+02 TIME STEP NUMBER 186 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19943E+01 0.37316E+01 Friction velocity uk : 0.19943E+01 0.37316E+01 Dimensionless distance yplus : 0.49858E-01 0.93290E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 168 0.21425E-03 0.72798E-10 0.37206E-04 c Velocity[X] 0.33852E-10 c Velocity[Y] 0.38945E-10 c Velocity[Z] 0.22928E-37 c Pressure 0.13833E-03 7 0.87752E-08 0.11348E-03 0.50349E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062559 0.062559 1.6737e-11 1.6737e-11 v Velocity[Z] -1.4601e-17 1.2229e-17 5.7733e-21 5.7733e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80359 39824 39824 v CourantNb 1.8205 19.976 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.187000000E+02 TIME STEP NUMBER 187 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666994E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19943E+01 0.37316E+01 Friction velocity uk : 0.19943E+01 0.37316E+01 Dimensionless distance yplus : 0.49859E-01 0.93290E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 166 0.20790E-03 0.68483E-10 0.36086E-04 c Velocity[X] 0.31854E-10 c Velocity[Y] 0.36629E-10 c Velocity[Z] 0.17708E-37 c Pressure 0.13421E-03 7 0.84816E-08 0.11009E-03 0.48775E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062548 0.062548 3.2405e-11 3.2405e-11 v Velocity[Z] -1.4481e-17 1.216e-17 3.9367e-21 3.9367e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80360 39824 39824 v CourantNb 1.8204 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.188000000E+02 TIME STEP NUMBER 188 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666994E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37316E+01 Friction velocity uk : 0.19944E+01 0.37316E+01 Dimensionless distance yplus : 0.49859E-01 0.93289E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 165 0.20174E-03 0.64425E-10 0.35001E-04 c Velocity[X] 0.29970E-10 c Velocity[Y] 0.34455E-10 c Velocity[Z] 0.15236E-37 c Pressure 0.13022E-03 7 0.89271E-08 0.10681E-03 0.47253E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062537 0.062537 -5.5855e-10 -5.5855e-10 v Velocity[Z] -1.4474e-17 1.2261e-17 7.5997e-21 7.5997e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80360 39824 39824 v CourantNb 1.8203 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.189000000E+02 TIME STEP NUMBER 189 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37316E+01 Friction velocity uk : 0.19944E+01 0.37316E+01 Dimensionless distance yplus : 0.49859E-01 0.93289E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 164 0.19577E-03 0.60604E-10 0.33947E-04 c Velocity[X] 0.28198E-10 c Velocity[Y] 0.32406E-10 c Velocity[Z] 0.33898E-37 c Pressure 0.12634E-03 7 0.85981E-08 0.10362E-03 0.45780E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062527 0.062527 -5.1025e-10 -5.1025e-10 v Velocity[Z] -1.4481e-17 1.2158e-17 4.1361e-21 4.1361e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80360 39824 39824 v CourantNb 1.8202 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.190000000E+02 TIME STEP NUMBER 190 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37315E+01 Friction velocity uk : 0.19944E+01 0.37315E+01 Dimensionless distance yplus : 0.49860E-01 0.93289E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 163 0.18997E-03 0.57013E-10 0.32926E-04 c Velocity[X] 0.26532E-10 c Velocity[Y] 0.30481E-10 c Velocity[Z] 0.28805E-37 c Pressure 0.12258E-03 7 0.82788E-08 0.10053E-03 0.44353E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062517 0.062517 -4.5608e-10 -4.5608e-10 v Velocity[Z] -1.4596e-17 1.2194e-17 6.3662e-21 6.3662e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80360 39824 39824 v CourantNb 1.8201 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.191000000E+02 TIME STEP NUMBER 191 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37315E+01 Friction velocity uk : 0.19944E+01 0.37315E+01 Dimensionless distance yplus : 0.49860E-01 0.93288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 162 0.18434E-03 0.53634E-10 0.31935E-04 c Velocity[X] 0.24965E-10 c Velocity[Y] 0.28669E-10 c Velocity[Z] 0.15597E-37 c Pressure 0.11894E-03 7 0.76504E-08 0.97528E-04 0.42966E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062508 0.062508 -4.3931e-11 -4.3931e-11 v Velocity[Z] -1.4597e-17 1.2249e-17 5.6647e-21 5.6647e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80360 39824 39824 v CourantNb 1.82 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.192000000E+02 TIME STEP NUMBER 192 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37315E+01 Friction velocity uk : 0.19944E+01 0.37315E+01 Dimensionless distance yplus : 0.49860E-01 0.93288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 161 0.17888E-03 0.50456E-10 0.30975E-04 c Velocity[X] 0.23491E-10 c Velocity[Y] 0.26965E-10 c Velocity[Z] 0.23884E-37 c Pressure 0.11540E-03 7 0.73861E-08 0.94619E-04 0.41632E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062498 0.062498 -2.1506e-11 -2.1506e-11 v Velocity[Z] -1.4481e-17 1.2161e-17 3.7709e-21 3.7709e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80361 39824 39824 v CourantNb 1.8199 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.193000000E+02 TIME STEP NUMBER 193 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37315E+01 Friction velocity uk : 0.19944E+01 0.37315E+01 Dimensionless distance yplus : 0.49860E-01 0.93288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 160 0.17358E-03 0.47467E-10 0.30043E-04 c Velocity[X] 0.22104E-10 c Velocity[Y] 0.25363E-10 c Velocity[Z] 0.22550E-37 c Pressure 0.11196E-03 7 0.71376E-08 0.91796E-04 0.40339E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062489 0.062489 3.324e-12 3.324e-12 v Velocity[Z] -1.4481e-17 1.2256e-17 3.9731e-21 3.9731e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80361 39824 39824 v CourantNb 1.8198 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.194000000E+02 TIME STEP NUMBER 194 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37315E+01 Friction velocity uk : 0.19944E+01 0.37315E+01 Dimensionless distance yplus : 0.49860E-01 0.93287E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 159 0.16844E-03 0.44655E-10 0.29140E-04 c Velocity[X] 0.20800E-10 c Velocity[Y] 0.23855E-10 c Velocity[Z] 0.12077E-37 c Pressure 0.10863E-03 7 0.67849E-08 0.89057E-04 0.39086E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099443 1.0009 0.66381 0.66381 v Velocity[Y] -0.062481 0.062481 1.6865e-10 1.6865e-10 v Velocity[Z] -1.4482e-17 1.2249e-17 6.7624e-21 6.7624e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80361 39824 39824 v CourantNb 1.8198 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.195000000E+02 TIME STEP NUMBER 195 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37315E+01 Friction velocity uk : 0.19944E+01 0.37315E+01 Dimensionless distance yplus : 0.49861E-01 0.93287E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 158 0.16345E-03 0.42010E-10 0.28264E-04 c Velocity[X] 0.19573E-10 c Velocity[Y] 0.22437E-10 c Velocity[Z] 0.11684E-37 c Pressure 0.10539E-03 7 0.65579E-08 0.86401E-04 0.37876E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099443 1.0009 0.66381 0.66381 v Velocity[Y] -0.062472 0.062472 1.7212e-10 1.7212e-10 v Velocity[Z] -1.4481e-17 1.2258e-17 6.4988e-21 6.4988e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80361 39824 39824 v CourantNb 1.8197 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.196000000E+02 TIME STEP NUMBER 196 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37315E+01 Friction velocity uk : 0.19944E+01 0.37315E+01 Dimensionless distance yplus : 0.49861E-01 0.93287E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 157 0.15860E-03 0.39522E-10 0.27414E-04 c Velocity[X] 0.18418E-10 c Velocity[Y] 0.21104E-10 c Velocity[Z] 0.19047E-37 c Pressure 0.10226E-03 7 0.62758E-08 0.83823E-04 0.36703E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062464 0.062464 2.3894e-10 2.3894e-10 v Velocity[Z] -1.4596e-17 1.2251e-17 4.4532e-21 4.4532e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80361 39824 39824 v CourantNb 1.8196 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.197000000E+02 TIME STEP NUMBER 197 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37315E+01 Friction velocity uk : 0.19944E+01 0.37315E+01 Dimensionless distance yplus : 0.49861E-01 0.93286E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62387E+01 156 0.15391E-03 0.37181E-10 0.26590E-04 c Velocity[X] 0.17332E-10 c Velocity[Y] 0.19850E-10 c Velocity[Z] 0.12245E-37 c Pressure 0.99211E-04 7 0.60332E-08 0.81323E-04 0.35567E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062456 0.062456 2.819e-10 2.819e-10 v Velocity[Z] -1.4478e-17 1.2247e-17 5.8006e-21 5.8006e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80362 39824 39824 v CourantNb 1.8195 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.198000000E+02 TIME STEP NUMBER 198 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37314E+01 Friction velocity uk : 0.19944E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93286E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 155 0.14934E-03 0.34980E-10 0.25790E-04 c Velocity[X] 0.16310E-10 c Velocity[Y] 0.18670E-10 c Velocity[Z] 0.18942E-37 c Pressure 0.96257E-04 7 0.58576E-08 0.78897E-04 0.34467E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062448 0.062448 2.694e-10 2.694e-10 v Velocity[Z] -1.4481e-17 1.2246e-17 6.3529e-21 6.3529e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80362 39824 39824 v CourantNb 1.8195 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.199000000E+02 TIME STEP NUMBER 199 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37314E+01 Friction velocity uk : 0.19944E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93286E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 154 0.14492E-03 0.32908E-10 0.25015E-04 c Velocity[X] 0.15348E-10 c Velocity[Y] 0.17560E-10 c Velocity[Z] 0.12741E-37 c Pressure 0.93391E-04 7 0.56633E-08 0.76543E-04 0.33404E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062441 0.062441 2.6641e-10 2.6641e-10 v Velocity[Z] -1.4542e-17 1.2191e-17 5.6282e-21 5.6282e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80362 39824 39824 v CourantNb 1.8194 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.200000000E+02 TIME STEP NUMBER 200 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37314E+01 Friction velocity uk : 0.19944E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93286E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 153 0.14062E-03 0.30960E-10 0.24263E-04 c Velocity[X] 0.14443E-10 c Velocity[Y] 0.16517E-10 c Velocity[Z] 0.16892E-37 c Pressure 0.90610E-04 7 0.54758E-08 0.74260E-04 0.32373E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062434 0.062434 2.63e-10 2.63e-10 v Velocity[Z] -1.4597e-17 1.2246e-17 3.2991e-21 3.2991e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80362 39824 39824 v CourantNb 1.8193 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.201000000E+02 TIME STEP NUMBER 201 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37314E+01 Friction velocity uk : 0.19944E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 152 0.13646E-03 0.29127E-10 0.23534E-04 c Velocity[X] 0.13592E-10 c Velocity[Y] 0.15535E-10 c Velocity[Z] 0.17827E-37 c Pressure 0.87912E-04 7 0.52950E-08 0.72045E-04 0.31375E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062427 0.062427 2.5926e-10 2.5926e-10 v Velocity[Z] -1.4529e-17 1.2256e-17 3.5748e-21 3.5748e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80362 39824 39824 v CourantNb 1.8193 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.202000000E+02 TIME STEP NUMBER 202 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37314E+01 Friction velocity uk : 0.19944E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 151 0.13241E-03 0.27403E-10 0.22827E-04 c Velocity[X] 0.12791E-10 c Velocity[Y] 0.14612E-10 c Velocity[Z] 0.15742E-37 c Pressure 0.85294E-04 7 0.51207E-08 0.69896E-04 0.30409E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.06242 0.06242 2.5527e-10 2.5527e-10 v Velocity[Z] -1.4517e-17 1.2251e-17 4.2436e-21 4.2436e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80362 39824 39824 v CourantNb 1.8192 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.203000000E+02 TIME STEP NUMBER 203 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37314E+01 Friction velocity uk : 0.19944E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 150 0.12849E-03 0.25781E-10 0.22141E-04 c Velocity[X] 0.12037E-10 c Velocity[Y] 0.13743E-10 c Velocity[Z] 0.23397E-37 c Pressure 0.82753E-04 7 0.49674E-08 0.67811E-04 0.29472E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062413 0.062413 2.4254e-10 2.4254e-10 v Velocity[Z] -1.4481e-17 1.2251e-17 3.3506e-21 3.3506e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80363 39824 39824 v CourantNb 1.8192 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.204000000E+02 TIME STEP NUMBER 204 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37314E+01 Friction velocity uk : 0.19945E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 149 0.12468E-03 0.24255E-10 0.21476E-04 c Velocity[X] 0.11329E-10 c Velocity[Y] 0.12926E-10 c Velocity[Z] 0.17098E-37 c Pressure 0.80289E-04 7 0.48960E-08 0.65788E-04 0.28561E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062407 0.062407 2.2137e-10 2.2137e-10 v Velocity[Z] -1.4481e-17 1.2188e-17 3.9406e-21 3.9406e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80363 39824 39824 v CourantNb 1.8191 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.205000000E+02 TIME STEP NUMBER 205 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37314E+01 Friction velocity uk : 0.19945E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 148 0.12098E-03 0.22819E-10 0.20831E-04 c Velocity[X] 0.10661E-10 c Velocity[Y] 0.12158E-10 c Velocity[Z] 0.15649E-37 c Pressure 0.77897E-04 7 0.47351E-08 0.63825E-04 0.27683E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.0624 0.0624 2.1074e-10 2.1074e-10 v Velocity[Z] -1.4482e-17 1.2159e-17 4.0635e-21 4.0635e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80363 39824 39824 v CourantNb 1.819 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.206000000E+02 TIME STEP NUMBER 206 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37314E+01 Friction velocity uk : 0.19945E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93284E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 147 0.11739E-03 0.21469E-10 0.20205E-04 c Velocity[X] 0.10033E-10 c Velocity[Y] 0.11435E-10 c Velocity[Z] 0.15842E-37 c Pressure 0.75577E-04 7 0.45650E-08 0.61921E-04 0.26832E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062394 0.062394 2.3879e-10 2.3879e-10 v Velocity[Z] -1.4596e-17 1.225e-17 6.0783e-21 6.0783e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80363 39824 39824 v CourantNb 1.819 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.207000000E+02 TIME STEP NUMBER 207 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37314E+01 Friction velocity uk : 0.19945E+01 0.37314E+01 Dimensionless distance yplus : 0.49861E-01 0.93284E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 146 0.11391E-03 0.20198E-10 0.19598E-04 c Velocity[X] 0.94425E-11 c Velocity[Y] 0.10756E-10 c Velocity[Z] 0.11340E-37 c Pressure 0.73326E-04 7 0.44113E-08 0.60074E-04 0.26009E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062389 0.062389 2.3648e-10 2.3648e-10 v Velocity[Z] -1.4554e-17 1.225e-17 5.4267e-21 5.4267e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80363 39824 39824 v CourantNb 1.8189 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.208000000E+02 TIME STEP NUMBER 208 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37314E+01 Friction velocity uk : 0.19945E+01 0.37314E+01 Dimensionless distance yplus : 0.49862E-01 0.93284E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 145 0.11054E-03 0.19003E-10 0.19009E-04 c Velocity[X] 0.88865E-11 c Velocity[Y] 0.10117E-10 c Velocity[Z] 0.15514E-37 c Pressure 0.71141E-04 7 0.42570E-08 0.58282E-04 0.25210E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062383 0.062383 2.3452e-10 2.3452e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.8853e-21 5.8853e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80363 39824 39824 v CourantNb 1.8189 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.209000000E+02 TIME STEP NUMBER 209 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666986E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49862E-01 0.93284E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 144 0.10726E-03 0.17879E-10 0.18438E-04 c Velocity[X] 0.83634E-11 c Velocity[Y] 0.95154E-11 c Velocity[Z] 0.34462E-37 c Pressure 0.69022E-04 7 0.41154E-08 0.56544E-04 0.24437E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062377 0.062377 2.3095e-10 2.3095e-10 v Velocity[Z] -1.4481e-17 1.225e-17 5.3905e-21 5.3905e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80363 39824 39824 v CourantNb 1.8188 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.210000000E+02 TIME STEP NUMBER 210 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49862E-01 0.93283E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 143 0.10408E-03 0.16820E-10 0.17884E-04 c Velocity[X] 0.78709E-11 c Velocity[Y] 0.89492E-11 c Velocity[Z] 0.24762E-37 c Pressure 0.66966E-04 6 0.99733E-08 0.54857E-04 0.23688E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062372 0.062372 2.7848e-10 2.7848e-10 v Velocity[Z] -1.4596e-17 1.225e-17 6.0276e-21 6.0276e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80363 39824 39824 v CourantNb 1.8188 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.211000000E+02 TIME STEP NUMBER 211 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666988E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49862E-01 0.93283E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 142 0.10099E-03 0.15816E-10 0.17342E-04 c Velocity[X] 0.73995E-11 c Velocity[Y] 0.84166E-11 c Velocity[Z] 0.16714E-37 c Pressure 0.64971E-04 9 0.94035E-08 0.53221E-04 0.22960E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062367 0.062367 1.4281e-09 1.4281e-09 v Velocity[Z] -1.4481e-17 1.216e-17 3.8362e-21 3.8362e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8188 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.212000000E+02 TIME STEP NUMBER 212 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49862E-01 0.93283E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 141 0.97997E-04 0.14890E-10 0.16827E-04 c Velocity[X] 0.69723E-11 c Velocity[Y] 0.79177E-11 c Velocity[Z] 0.19522E-37 c Pressure 0.63035E-04 9 0.91113E-08 0.51633E-04 0.22258E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062362 0.062362 1.3849e-09 1.3849e-09 v Velocity[Z] -1.448e-17 1.2169e-17 5.2331e-21 5.2331e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8187 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.213000000E+02 TIME STEP NUMBER 213 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49862E-01 0.93283E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 140 0.95091E-04 0.14010E-10 0.16322E-04 c Velocity[X] 0.65622E-11 c Velocity[Y] 0.74474E-11 c Velocity[Z] 0.22267E-37 c Pressure 0.61157E-04 9 0.88279E-08 0.50093E-04 0.21576E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062357 0.062357 1.3357e-09 1.3357e-09 v Velocity[Z] -1.4597e-17 1.2232e-17 5.557e-21 5.557e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8187 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.214000000E+02 TIME STEP NUMBER 214 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49862E-01 0.93283E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 139 0.92270E-04 0.13180E-10 0.15831E-04 c Velocity[X] 0.61757E-11 c Velocity[Y] 0.70045E-11 c Velocity[Z] 0.12805E-37 c Pressure 0.59335E-04 9 0.85149E-08 0.48599E-04 0.20914E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062352 0.062352 1.197e-09 1.197e-09 v Velocity[Z] -1.4598e-17 1.2228e-17 6.6623e-21 6.6623e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8186 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.215000000E+02 TIME STEP NUMBER 215 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666982E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49862E-01 0.93283E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 139 0.89534E-04 0.12396E-10 0.15353E-04 c Velocity[X] 0.58081E-11 c Velocity[Y] 0.65880E-11 c Velocity[Z] 0.19180E-37 c Pressure 0.57567E-04 8 0.98356E-08 0.47149E-04 0.20275E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062348 0.062348 1.4966e-09 1.4966e-09 v Velocity[Z] -1.46e-17 1.2195e-17 8.2601e-21 8.2601e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8186 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.216000000E+02 TIME STEP NUMBER 216 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666983E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49862E-01 0.93282E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 138 0.86878E-04 0.11668E-10 0.14896E-04 c Velocity[X] 0.54710E-11 c Velocity[Y] 0.61975E-11 c Velocity[Z] 0.28919E-37 c Pressure 0.55851E-04 8 0.95379E-08 0.45742E-04 0.19655E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062343 0.062343 1.4541e-09 1.4541e-09 v Velocity[Z] -1.4491e-17 1.2257e-17 3.9191e-21 3.9191e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8186 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.217000000E+02 TIME STEP NUMBER 217 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666984E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49861E-01 0.93282E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 137 0.84301E-04 0.10978E-10 0.14448E-04 c Velocity[X] 0.51495E-11 c Velocity[Y] 0.58287E-11 c Velocity[Z] 0.15025E-37 c Pressure 0.54187E-04 8 0.92495E-08 0.44378E-04 0.19055E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062339 0.062339 1.4147e-09 1.4147e-09 v Velocity[Z] -1.4596e-17 1.2251e-17 5.9847e-21 5.9847e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8185 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.218000000E+02 TIME STEP NUMBER 218 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666985E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49861E-01 0.93282E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 136 0.81800E-04 0.10330E-10 0.14015E-04 c Velocity[X] 0.48472E-11 c Velocity[Y] 0.54825E-11 c Velocity[Z] 0.71486E-38 c Pressure 0.52572E-04 8 0.90496E-08 0.43054E-04 0.18469E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099447 1.0009 0.66381 0.66381 v Velocity[Y] -0.062335 0.062335 1.5548e-09 1.5548e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.7281e-21 6.7281e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8185 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.219000000E+02 TIME STEP NUMBER 219 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666987E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49861E-01 0.93282E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 135 0.79374E-04 0.97182E-11 0.13594E-04 c Velocity[X] 0.45616E-11 c Velocity[Y] 0.51566E-11 c Velocity[Z] 0.19930E-37 c Pressure 0.51005E-04 8 0.87727E-08 0.41770E-04 0.17906E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062331 0.062331 1.501e-09 1.501e-09 v Velocity[Z] -1.4481e-17 1.2195e-17 5.9686e-21 5.9686e-21 v ǁVelocityǁ 0.099447 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8185 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.220000000E+02 TIME STEP NUMBER 220 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666988E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49861E-01 0.93282E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 134 0.77019E-04 0.91436E-11 0.13186E-04 c Velocity[X] 0.42934E-11 c Velocity[Y] 0.48502E-11 c Velocity[Z] 0.12282E-37 c Pressure 0.49485E-04 8 0.85044E-08 0.40524E-04 0.17360E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062327 0.062327 1.4444e-09 1.4444e-09 v Velocity[Z] -1.4596e-17 1.225e-17 5.4019e-21 5.4019e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80364 39824 39824 v CourantNb 1.8184 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.221000000E+02 TIME STEP NUMBER 221 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49861E-01 0.93282E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 133 0.74734E-04 0.86030E-11 0.12790E-04 c Velocity[X] 0.40410E-11 c Velocity[Y] 0.45620E-11 c Velocity[Z] 0.20860E-37 c Pressure 0.48010E-04 8 0.82443E-08 0.39315E-04 0.16830E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062323 0.062323 1.3946e-09 1.3946e-09 v Velocity[Z] -1.4597e-17 1.225e-17 4.7073e-21 4.7073e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8184 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.222000000E+02 TIME STEP NUMBER 222 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49861E-01 0.93282E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 132 0.72516E-04 0.80964E-11 0.12408E-04 c Velocity[X] 0.38038E-11 c Velocity[Y] 0.42927E-11 c Velocity[Z] 0.10196E-37 c Pressure 0.46579E-04 7 0.98757E-08 0.38142E-04 0.16317E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.06232 0.06232 1.6598e-09 1.6598e-09 v Velocity[Z] -1.4598e-17 1.2251e-17 6.6247e-21 6.6247e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8184 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.223000000E+02 TIME STEP NUMBER 223 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 131 0.70365E-04 0.76156E-11 0.12034E-04 c Velocity[X] 0.35796E-11 c Velocity[Y] 0.40360E-11 c Velocity[Z] 0.41762E-37 c Pressure 0.45191E-04 7 0.95554E-08 0.37004E-04 0.15819E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062316 0.062316 1.6065e-09 1.6065e-09 v Velocity[Z] -1.4481e-17 1.2198e-17 3.9254e-21 3.9254e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8183 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.224000000E+02 TIME STEP NUMBER 224 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37313E+01 Friction velocity uk : 0.19945E+01 0.37313E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 130 0.68276E-04 0.71656E-11 0.11673E-04 c Velocity[X] 0.33695E-11 c Velocity[Y] 0.37961E-11 c Velocity[Z] 0.21413E-37 c Pressure 0.43844E-04 7 0.92502E-08 0.35900E-04 0.15337E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062313 0.062313 1.5515e-09 1.5515e-09 v Velocity[Z] -1.4473e-17 1.2246e-17 5.1472e-21 5.1472e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8183 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.225000000E+02 TIME STEP NUMBER 225 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37312E+01 Friction velocity uk : 0.19945E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 129 0.66250E-04 0.67420E-11 0.11323E-04 c Velocity[X] 0.31715E-11 c Velocity[Y] 0.35706E-11 c Velocity[Z] 0.24794E-37 c Pressure 0.42537E-04 7 0.89508E-08 0.34829E-04 0.14870E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062309 0.062309 1.5015e-09 1.5015e-09 v Velocity[Z] -1.4481e-17 1.2222e-17 6.333e-21 6.333e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8183 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.226000000E+02 TIME STEP NUMBER 226 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37312E+01 Friction velocity uk : 0.19945E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 129 0.64284E-04 0.63447E-11 0.10984E-04 c Velocity[X] 0.29845E-11 c Velocity[Y] 0.33602E-11 c Velocity[Z] 0.25591E-37 c Pressure 0.41269E-04 6 0.99833E-08 0.33790E-04 0.14417E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062306 0.062306 1.6836e-09 1.6836e-09 v Velocity[Z] -1.4477e-17 1.2261e-17 4.7289e-21 4.7289e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8183 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.227000000E+02 TIME STEP NUMBER 227 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666994E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19945E+01 0.37312E+01 Friction velocity uk : 0.19945E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 128 0.62375E-04 0.59685E-11 0.10653E-04 c Velocity[X] 0.28095E-11 c Velocity[Y] 0.31590E-11 c Velocity[Z] 0.12959E-37 c Pressure 0.40039E-04 6 0.96471E-08 0.32782E-04 0.13978E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.062303 0.062303 1.6275e-09 1.6275e-09 v Velocity[Z] -1.4483e-17 1.2188e-17 7.3529e-21 7.3529e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8182 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.228000000E+02 TIME STEP NUMBER 228 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666995E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 127 0.60524E-04 0.56157E-11 0.10334E-04 c Velocity[X] 0.26446E-11 c Velocity[Y] 0.29712E-11 c Velocity[Z] 0.17482E-37 c Pressure 0.38845E-04 6 0.93232E-08 0.31804E-04 0.13553E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099446 1.0009 0.66381 0.66381 v Velocity[Y] -0.0623 0.0623 1.5736e-09 1.5736e-09 v Velocity[Z] -1.4596e-17 1.225e-17 4.8582e-21 4.8582e-21 v ǁVelocityǁ 0.099446 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8182 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.229000000E+02 TIME STEP NUMBER 229 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666995E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 126 0.58727E-04 0.52839E-11 0.10024E-04 c Velocity[X] 0.24892E-11 c Velocity[Y] 0.27946E-11 c Velocity[Z] 0.11413E-37 c Pressure 0.37687E-04 6 0.90105E-08 0.30855E-04 0.13140E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062297 0.062297 1.5218e-09 1.5218e-09 v Velocity[Z] -1.4597e-17 1.225e-17 2.7037e-21 2.7037e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8182 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.230000000E+02 TIME STEP NUMBER 230 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666996E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 125 0.56984E-04 0.49717E-11 0.97230E-05 c Velocity[X] 0.23431E-11 c Velocity[Y] 0.26286E-11 c Velocity[Z] 0.22774E-37 c Pressure 0.36564E-04 6 0.86748E-08 0.29935E-04 0.12740E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062294 0.062294 1.4918e-09 1.4918e-09 v Velocity[Z] -1.4597e-17 1.225e-17 4.9455e-21 4.9455e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8182 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.231000000E+02 TIME STEP NUMBER 231 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666996E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 124 0.55293E-04 0.46778E-11 0.94313E-05 c Velocity[X] 0.22054E-11 c Velocity[Y] 0.24724E-11 c Velocity[Z] 0.40431E-37 c Pressure 0.35474E-04 6 0.83857E-08 0.29042E-04 0.12353E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062291 0.062291 1.443e-09 1.443e-09 v Velocity[Z] -1.4553e-17 1.225e-17 3.0851e-21 3.0851e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8181 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.232000000E+02 TIME STEP NUMBER 232 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666996E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 123 0.53651E-04 0.44014E-11 0.91484E-05 c Velocity[X] 0.20758E-11 c Velocity[Y] 0.23256E-11 c Velocity[Z] 0.17035E-37 c Pressure 0.34416E-04 6 0.81123E-08 0.28175E-04 0.11977E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062288 0.062288 1.3892e-09 1.3892e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.0111e-21 5.0111e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8181 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.233000000E+02 TIME STEP NUMBER 233 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666997E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 123 0.52059E-04 0.41409E-11 0.88736E-05 c Velocity[X] 0.19530E-11 c Velocity[Y] 0.21880E-11 c Velocity[Z] 0.11789E-37 c Pressure 0.33390E-04 6 0.78451E-08 0.27335E-04 0.11613E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062286 0.062286 1.3445e-09 1.3445e-09 v Velocity[Z] -1.4602e-17 1.225e-17 5.514e-21 5.514e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8181 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.234000000E+02 TIME STEP NUMBER 234 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 122 0.50513E-04 0.38966E-11 0.86078E-05 c Velocity[X] 0.18392E-11 c Velocity[Y] 0.20575E-11 c Velocity[Z] 0.10211E-37 c Pressure 0.32394E-04 6 0.75884E-08 0.26519E-04 0.11260E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062283 0.062283 1.2974e-09 1.2974e-09 v Velocity[Z] -1.4597e-17 1.225e-17 3.9761e-21 3.9761e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.8181 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.235000000E+02 TIME STEP NUMBER 235 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 121 0.49014E-04 0.36664E-11 0.83497E-05 c Velocity[X] 0.17311E-11 c Velocity[Y] 0.19353E-11 c Velocity[Z] 0.17756E-37 c Pressure 0.31429E-04 6 0.73359E-08 0.25728E-04 0.10918E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062281 0.062281 1.2559e-09 1.2559e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.7173e-21 5.7173e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80365 39824 39824 v CourantNb 1.818 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.236000000E+02 TIME STEP NUMBER 236 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666998E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 120 0.47559E-04 0.34498E-11 0.80993E-05 c Velocity[X] 0.16295E-11 c Velocity[Y] 0.18203E-11 c Velocity[Z] 0.67637E-38 c Pressure 0.30491E-04 6 0.71004E-08 0.24960E-04 0.10586E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062278 0.062278 1.2108e-09 1.2108e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.6794e-21 6.6794e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.818 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.237000000E+02 TIME STEP NUMBER 237 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666999E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 119 0.46146E-04 0.32460E-11 0.78564E-05 c Velocity[X] 0.15338E-11 c Velocity[Y] 0.17122E-11 c Velocity[Z] 0.20611E-37 c Pressure 0.29582E-04 6 0.68920E-08 0.24216E-04 0.10264E-05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099445 1.0009 0.66381 0.66381 v Velocity[Y] -0.062276 0.062276 1.1729e-09 1.1729e-09 v Velocity[Z] -1.4597e-17 1.225e-17 7.3721e-21 7.3721e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.818 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.238000000E+02 TIME STEP NUMBER 238 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 118 0.44776E-04 0.30542E-11 0.76208E-05 c Velocity[X] 0.14437E-11 c Velocity[Y] 0.16105E-11 c Velocity[Z] 0.45233E-37 c Pressure 0.28700E-04 6 0.66631E-08 0.23493E-04 0.99527E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062274 0.062274 1.1354e-09 1.1354e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.9093e-21 6.9093e-21 v ǁVelocityǁ 0.099445 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.818 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.239000000E+02 TIME STEP NUMBER 239 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 117 0.43447E-04 0.28738E-11 0.73923E-05 c Velocity[X] 0.13590E-11 c Velocity[Y] 0.15149E-11 c Velocity[Z] 0.15045E-37 c Pressure 0.27844E-04 6 0.64296E-08 0.22792E-04 0.96506E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062272 0.062272 1.1014e-09 1.1014e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.7259e-21 5.7259e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.818 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.240000000E+02 TIME STEP NUMBER 240 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 117 0.42157E-04 0.27037E-11 0.71702E-05 c Velocity[X] 0.12784E-11 c Velocity[Y] 0.14253E-11 c Velocity[Z] 0.30069E-37 c Pressure 0.27014E-04 6 0.62308E-08 0.22112E-04 0.93579E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.06227 0.06227 1.0663e-09 1.0663e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.625e-21 5.625e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.818 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.241000000E+02 TIME STEP NUMBER 241 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 116 0.40905E-04 0.25443E-11 0.69556E-05 c Velocity[X] 0.12041E-11 c Velocity[Y] 0.13403E-11 c Velocity[Z] 0.21775E-37 c Pressure 0.26208E-04 6 0.60243E-08 0.21453E-04 0.90739E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062268 0.062268 1.0325e-09 1.0325e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.2392e-21 6.2392e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8179 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.242000000E+02 TIME STEP NUMBER 242 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 115 0.39690E-04 0.23941E-11 0.67471E-05 c Velocity[X] 0.11334E-11 c Velocity[Y] 0.12607E-11 c Velocity[Z] 0.12218E-37 c Pressure 0.25427E-04 6 0.58695E-08 0.20812E-04 0.87984E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062266 0.062266 9.9518e-10 9.9518e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5361e-21 5.5361e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8179 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.243000000E+02 TIME STEP NUMBER 243 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 114 0.38511E-04 0.22527E-11 0.65448E-05 c Velocity[X] 0.10669E-11 c Velocity[Y] 0.11858E-11 c Velocity[Z] 0.14685E-37 c Pressure 0.24668E-04 6 0.56965E-08 0.20191E-04 0.85314E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062264 0.062264 9.5753e-10 9.5753e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.6273e-21 4.6273e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8179 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.244000000E+02 TIME STEP NUMBER 244 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93280E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 113 0.37367E-04 0.21195E-11 0.63485E-05 c Velocity[X] 0.10042E-11 c Velocity[Y] 0.11153E-11 c Velocity[Z] 0.13461E-37 c Pressure 0.23933E-04 6 0.55032E-08 0.19589E-04 0.82721E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062262 0.062262 9.1775e-10 9.1775e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.1133e-21 7.1133e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8179 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.245000000E+02 TIME STEP NUMBER 245 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 113 0.36258E-04 0.19941E-11 0.61578E-05 c Velocity[X] 0.94460E-12 c Velocity[Y] 0.10495E-11 c Velocity[Z] 0.22025E-37 c Pressure 0.23219E-04 6 0.53253E-08 0.19005E-04 0.80216E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.06226 0.06226 8.8848e-10 8.8848e-10 v Velocity[Z] -1.4477e-17 1.2251e-17 6.7943e-21 6.7943e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8179 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.246000000E+02 TIME STEP NUMBER 246 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 112 0.35181E-04 0.18766E-11 0.59737E-05 c Velocity[X] 0.88981E-12 c Velocity[Y] 0.98684E-12 c Velocity[Z] 0.22515E-37 c Pressure 0.22526E-04 6 0.51498E-08 0.18437E-04 0.77784E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099444 1.0009 0.66381 0.66381 v Velocity[Y] -0.062258 0.062258 8.6029e-10 8.6029e-10 v Velocity[Z] -1.4596e-17 1.225e-17 5.1869e-21 5.1869e-21 v ǁVelocityǁ 0.099444 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8179 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.247000000E+02 TIME STEP NUMBER 247 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 111 0.34136E-04 0.17658E-11 0.57946E-05 c Velocity[X] 0.83758E-12 c Velocity[Y] 0.92824E-12 c Velocity[Z] 0.14039E-37 c Pressure 0.21855E-04 6 0.49800E-08 0.17887E-04 0.75426E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099443 1.0009 0.66381 0.66381 v Velocity[Y] -0.062257 0.062257 8.33e-10 8.33e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.1214e-21 6.1214e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8179 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.248000000E+02 TIME STEP NUMBER 248 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 110 0.33122E-04 0.16616E-11 0.56209E-05 c Velocity[X] 0.78842E-12 c Velocity[Y] 0.87313E-12 c Velocity[Z] 0.18594E-37 c Pressure 0.21203E-04 6 0.48159E-08 0.17354E-04 0.73139E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099443 1.0009 0.66381 0.66381 v Velocity[Y] -0.062255 0.062255 8.0654e-10 8.0654e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.5316e-21 3.5316e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.249000000E+02 TIME STEP NUMBER 249 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 109 0.32138E-04 0.15634E-11 0.54524E-05 c Velocity[X] 0.74215E-12 c Velocity[Y] 0.82129E-12 c Velocity[Z] 0.21839E-37 c Pressure 0.20570E-04 6 0.46574E-08 0.16836E-04 0.70923E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099443 1.0009 0.66381 0.66381 v Velocity[Y] -0.062253 0.062253 7.809e-10 7.809e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.7856e-21 6.7856e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.250000000E+02 TIME STEP NUMBER 250 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 250, Physical time 0.25000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 250: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 109 0.31183E-04 0.14709E-11 0.52885E-05 c Velocity[X] 0.69799E-12 c Velocity[Y] 0.77287E-12 c Velocity[Z] 0.84518E-38 c Pressure 0.19957E-04 6 0.45071E-08 0.16333E-04 0.68777E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099443 1.0009 0.66381 0.66381 v Velocity[Y] -0.062252 0.062252 7.5618e-10 7.5618e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.2844e-21 7.2844e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.251000000E+02 TIME STEP NUMBER 251 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 108 0.30257E-04 0.13842E-11 0.51305E-05 c Velocity[X] 0.65759E-12 c Velocity[Y] 0.72666E-12 c Velocity[Z] 0.17946E-37 c Pressure 0.19361E-04 6 0.44198E-08 0.15846E-04 0.66691E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099443 1.0009 0.66381 0.66381 v Velocity[Y] -0.06225 0.06225 7.2267e-10 7.2267e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.4636e-21 5.4636e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.252000000E+02 TIME STEP NUMBER 252 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49861E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 107 0.29358E-04 0.13025E-11 0.49767E-05 c Velocity[X] 0.61901E-12 c Velocity[Y] 0.68351E-12 c Velocity[Z] 0.33434E-37 c Pressure 0.18784E-04 6 0.42745E-08 0.15373E-04 0.64671E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099443 1.0009 0.66381 0.66381 v Velocity[Y] -0.062249 0.062249 6.9956e-10 6.9956e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.57e-21 5.57e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.253000000E+02 TIME STEP NUMBER 253 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 106 0.28485E-04 0.12283E-11 0.48328E-05 c Velocity[X] 0.58459E-12 c Velocity[Y] 0.64368E-12 c Velocity[Z] 0.30052E-37 c Pressure 0.18224E-04 7 0.99158E-08 0.14914E-04 0.62698E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062247 0.062247 1.6607e-09 1.6607e-09 v Velocity[Z] -1.4597e-17 1.225e-17 7.0001e-21 7.0001e-21 v ǁVelocityǁ 0.099443 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.254000000E+02 TIME STEP NUMBER 254 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667003E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 105 0.27640E-04 0.11535E-11 0.46835E-05 c Velocity[X] 0.54891E-12 c Velocity[Y] 0.60464E-12 c Velocity[Z] 0.17891E-37 c Pressure 0.17680E-04 7 0.96216E-08 0.14469E-04 0.60747E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062246 0.062246 1.6252e-09 1.6252e-09 v Velocity[Z] -1.4601e-17 1.225e-17 3.593e-21 3.593e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.255000000E+02 TIME STEP NUMBER 255 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 105 0.26818E-04 0.10853E-11 0.45427E-05 c Velocity[X] 0.51607E-12 c Velocity[Y] 0.56920E-12 c Velocity[Z] 0.16340E-37 c Pressure 0.17153E-04 7 0.92958E-08 0.14038E-04 0.58970E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062245 0.062245 1.5623e-09 1.5623e-09 v Velocity[Z] -1.4478e-17 1.2231e-17 4.7159e-21 4.7159e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.256000000E+02 TIME STEP NUMBER 256 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 104 0.26021E-04 0.10214E-11 0.44070E-05 c Velocity[X] 0.48627E-12 c Velocity[Y] 0.53510E-12 c Velocity[Z] 0.13492E-37 c Pressure 0.16641E-04 7 0.90214E-08 0.13619E-04 0.57126E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062243 0.062243 1.5402e-09 1.5402e-09 v Velocity[Z] -1.4476e-17 1.2256e-17 3.2256e-21 3.2256e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8178 19.977 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.257000000E+02 TIME STEP NUMBER 257 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 103 0.25248E-04 0.96113E-12 0.42750E-05 c Velocity[X] 0.45779E-12 c Velocity[Y] 0.50334E-12 c Velocity[Z] 0.13136E-37 c Pressure 0.16144E-04 7 0.87108E-08 0.13212E-04 0.55457E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062242 0.062242 1.4656e-09 1.4656e-09 v Velocity[Z] -1.4484e-17 1.2254e-17 4.1089e-21 4.1089e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.258000000E+02 TIME STEP NUMBER 258 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667002E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37312E+01 Friction velocity uk : 0.19944E+01 0.37312E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 102 0.24497E-04 0.90335E-12 0.41446E-05 c Velocity[X] 0.43050E-12 c Velocity[Y] 0.47285E-12 c Velocity[Z] 0.14885E-37 c Pressure 0.15663E-04 6 0.98742E-08 0.12818E-04 0.53721E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062241 0.062241 1.8996e-09 1.8996e-09 v Velocity[Z] -1.4485e-17 1.2262e-17 5.2372e-21 5.2372e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.259000000E+02 TIME STEP NUMBER 259 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 102 0.23769E-04 0.85059E-12 0.40217E-05 c Velocity[X] 0.40487E-12 c Velocity[Y] 0.44572E-12 c Velocity[Z] 0.12486E-37 c Pressure 0.15196E-04 6 0.95725E-08 0.12435E-04 0.52101E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.06224 0.06224 1.8393e-09 1.8393e-09 v Velocity[Z] -1.4469e-17 1.2251e-17 6.3593e-21 6.3593e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.260000000E+02 TIME STEP NUMBER 260 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 101 0.23063E-04 0.80091E-12 0.39025E-05 c Velocity[X] 0.38197E-12 c Velocity[Y] 0.41894E-12 c Velocity[Z] 0.29116E-37 c Pressure 0.14742E-04 6 0.92516E-08 0.12064E-04 0.50583E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099442 1.0009 0.66381 0.66381 v Velocity[Y] -0.062239 0.062239 1.7483e-09 1.7483e-09 v Velocity[Z] -1.4596e-17 1.2251e-17 2.6592e-21 2.6592e-21 v ǁVelocityǁ 0.099442 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.261000000E+02 TIME STEP NUMBER 261 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 100 0.22377E-04 0.75333E-12 0.37848E-05 c Velocity[X] 0.35939E-12 c Velocity[Y] 0.39394E-12 c Velocity[Z] 0.23634E-37 c Pressure 0.14302E-04 5 0.98586E-08 0.11704E-04 0.48995E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062237 0.062238 2.0057e-09 2.0057e-09 v Velocity[Z] -1.4475e-17 1.2196e-17 2.3442e-21 2.3442e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.262000000E+02 TIME STEP NUMBER 262 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 99 0.21713E-04 0.70905E-12 0.36719E-05 c Velocity[X] 0.33845E-12 c Velocity[Y] 0.37061E-12 c Velocity[Z] 0.20783E-37 c Pressure 0.13876E-04 5 0.95507E-08 0.11355E-04 0.47569E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062236 0.062236 1.9094e-09 1.9094e-09 v Velocity[Z] -1.4473e-17 1.2256e-17 4.2513e-21 4.2513e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.263000000E+02 TIME STEP NUMBER 263 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666667001E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 99 0.21067E-04 0.66704E-12 0.35614E-05 c Velocity[X] 0.31813E-12 c Velocity[Y] 0.34892E-12 c Velocity[Z] 0.12998E-37 c Pressure 0.13462E-04 5 0.92719E-08 0.11016E-04 0.46079E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062235 0.062235 1.8795e-09 1.8795e-09 v Velocity[Z] -1.4596e-17 1.2251e-17 5.9827e-21 5.9827e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.264000000E+02 TIME STEP NUMBER 264 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 98 0.20441E-04 0.62759E-12 0.34545E-05 c Velocity[X] 0.29961E-12 c Velocity[Y] 0.32798E-12 c Velocity[Z] 0.11889E-37 c Pressure 0.13060E-04 5 0.89891E-08 0.10687E-04 0.44688E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062234 0.062234 1.8205e-09 1.8205e-09 v Velocity[Z] -1.4597e-17 1.2251e-17 4.5603e-21 4.5603e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.265000000E+02 TIME STEP NUMBER 265 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 97 0.19834E-04 0.59058E-12 0.33511E-05 c Velocity[X] 0.28205E-12 c Velocity[Y] 0.30853E-12 c Velocity[Z] 0.16857E-37 c Pressure 0.12670E-04 5 0.87211E-08 0.10368E-04 0.43334E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062233 0.062233 1.7606e-09 1.7606e-09 v Velocity[Z] -1.4597e-17 1.225e-17 4.1029e-21 4.1029e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80366 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.266000000E+02 TIME STEP NUMBER 266 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 96 0.19244E-04 0.55569E-12 0.32506E-05 c Velocity[X] 0.26548E-12 c Velocity[Y] 0.29021E-12 c Velocity[Z] 0.18195E-37 c Pressure 0.12292E-04 5 0.84577E-08 0.10059E-04 0.42025E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062232 0.062232 1.6903e-09 1.6903e-09 v Velocity[Z] -1.4597e-17 1.225e-17 7.6803e-21 7.6803e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.267000000E+02 TIME STEP NUMBER 267 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 96 0.18672E-04 0.52272E-12 0.31527E-05 c Velocity[X] 0.24951E-12 c Velocity[Y] 0.27321E-12 c Velocity[Z] 0.16878E-37 c Pressure 0.11925E-04 5 0.82022E-08 0.97587E-05 0.40759E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062232 0.062232 1.6307e-09 1.6307e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.7852e-21 5.7852e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.268000000E+02 TIME STEP NUMBER 268 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 95 0.18117E-04 0.49204E-12 0.30588E-05 c Velocity[X] 0.23526E-12 c Velocity[Y] 0.25678E-12 c Velocity[Z] 0.14233E-37 c Pressure 0.11569E-04 5 0.79522E-08 0.94674E-05 0.39528E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099441 1.0009 0.66381 0.66381 v Velocity[Y] -0.062231 0.062231 1.5721e-09 1.5721e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.3889e-21 6.3889e-21 v ǁVelocityǁ 0.099441 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.269000000E+02 TIME STEP NUMBER 269 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 94 0.17578E-04 0.46300E-12 0.29672E-05 c Velocity[X] 0.22146E-12 c Velocity[Y] 0.24154E-12 c Velocity[Z] 0.27587E-37 c Pressure 0.11224E-04 5 0.77088E-08 0.91849E-05 0.38334E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.06223 0.06223 1.5183e-09 1.5183e-09 v Velocity[Z] -1.4597e-17 1.225e-17 2.8891e-21 2.8891e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8177 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.270000000E+02 TIME STEP NUMBER 270 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 93 0.17056E-04 0.43568E-12 0.28783E-05 c Velocity[X] 0.20848E-12 c Velocity[Y] 0.22721E-12 c Velocity[Z] 0.23520E-37 c Pressure 0.10889E-04 5 0.74731E-08 0.89107E-05 0.37177E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062229 0.062229 1.4678e-09 1.4678e-09 v Velocity[Z] -1.4597e-17 1.225e-17 3.7952e-21 3.7952e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.271000000E+02 TIME STEP NUMBER 271 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 93 0.16548E-04 0.40981E-12 0.27915E-05 c Velocity[X] 0.19588E-12 c Velocity[Y] 0.21393E-12 c Velocity[Z] 0.94859E-38 c Pressure 0.10564E-04 5 0.72477E-08 0.86447E-05 0.36057E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062228 0.062228 1.4175e-09 1.4175e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.695e-21 6.695e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.272000000E+02 TIME STEP NUMBER 272 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 92 0.16056E-04 0.38578E-12 0.27084E-05 c Velocity[X] 0.18474E-12 c Velocity[Y] 0.20104E-12 c Velocity[Z] 0.15982E-37 c Pressure 0.10249E-04 5 0.70268E-08 0.83867E-05 0.34968E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062227 0.062227 1.3675e-09 1.3675e-09 v Velocity[Z] -1.4597e-17 1.225e-17 4.7739e-21 4.7739e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.273000000E+02 TIME STEP NUMBER 273 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 91 0.15579E-04 0.36302E-12 0.26273E-05 c Velocity[X] 0.17391E-12 c Velocity[Y] 0.18911E-12 c Velocity[Z] 0.15926E-37 c Pressure 0.99432E-05 5 0.68127E-08 0.81364E-05 0.33912E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062227 0.062227 1.3193e-09 1.3193e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.2641e-21 5.2641e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.274000000E+02 TIME STEP NUMBER 274 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 91 0.15116E-04 0.34145E-12 0.25481E-05 c Velocity[X] 0.16337E-12 c Velocity[Y] 0.17808E-12 c Velocity[Z] 0.12722E-37 c Pressure 0.96464E-05 5 0.66075E-08 0.78935E-05 0.32891E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062226 0.062226 1.2741e-09 1.2741e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.3985e-21 5.3985e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.275000000E+02 TIME STEP NUMBER 275 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 90 0.14666E-04 0.32144E-12 0.24723E-05 c Velocity[X] 0.15411E-12 c Velocity[Y] 0.16733E-12 c Velocity[Z] 0.13399E-37 c Pressure 0.93585E-05 5 0.64062E-08 0.76579E-05 0.31898E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062225 0.062225 1.2292e-09 1.2292e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.0689e-21 5.0689e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.276000000E+02 TIME STEP NUMBER 276 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 89 0.14230E-04 0.30248E-12 0.23983E-05 c Velocity[X] 0.14508E-12 c Velocity[Y] 0.15740E-12 c Velocity[Z] 0.21472E-37 c Pressure 0.90792E-05 5 0.62105E-08 0.74293E-05 0.30934E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062224 0.062224 1.1832e-09 1.1832e-09 v Velocity[Z] -1.4597e-17 1.225e-17 3.7495e-21 3.7495e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.277000000E+02 TIME STEP NUMBER 277 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 88 0.13807E-04 0.28463E-12 0.23264E-05 c Velocity[X] 0.13657E-12 c Velocity[Y] 0.14806E-12 c Velocity[Z] 0.12863E-37 c Pressure 0.88083E-05 5 0.60214E-08 0.72075E-05 0.30000E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062224 0.062224 1.1416e-09 1.1416e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.1289e-21 6.1289e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.278000000E+02 TIME STEP NUMBER 278 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 88 0.13396E-04 0.26770E-12 0.22562E-05 c Velocity[X] 0.12825E-12 c Velocity[Y] 0.13945E-12 c Velocity[Z] 0.12795E-37 c Pressure 0.85454E-05 5 0.58404E-08 0.69924E-05 0.29097E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062223 0.062223 1.1029e-09 1.1029e-09 v Velocity[Z] -1.4597e-17 1.225e-17 5.2472e-21 5.2472e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.279000000E+02 TIME STEP NUMBER 279 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 87 0.12998E-04 0.25203E-12 0.21891E-05 c Velocity[X] 0.12102E-12 c Velocity[Y] 0.13101E-12 c Velocity[Z] 0.15263E-37 c Pressure 0.82903E-05 5 0.56703E-08 0.67836E-05 0.28218E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.09944 1.0009 0.66381 0.66381 v Velocity[Y] -0.062222 0.062222 1.069e-09 1.069e-09 v Velocity[Z] -1.4597e-17 1.225e-17 6.3729e-21 6.3729e-21 v ǁVelocityǁ 0.09944 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.280000000E+02 TIME STEP NUMBER 280 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 86 0.12612E-04 0.23717E-12 0.21236E-05 c Velocity[X] 0.11393E-12 c Velocity[Y] 0.12324E-12 c Velocity[Z] 0.11043E-37 c Pressure 0.80429E-05 5 0.54978E-08 0.65811E-05 0.27366E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062222 0.062222 1.0319e-09 1.0319e-09 v Velocity[Z] -1.4597e-17 1.225e-17 4.8976e-21 4.8976e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.281000000E+02 TIME STEP NUMBER 281 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 86 0.12236E-04 0.22305E-12 0.20594E-05 c Velocity[X] 0.10696E-12 c Velocity[Y] 0.11609E-12 c Velocity[Z] 0.19302E-37 c Pressure 0.78028E-05 5 0.53328E-08 0.63847E-05 0.26543E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062221 0.062221 9.9735e-10 9.9735e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.0897e-21 7.0897e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.282000000E+02 TIME STEP NUMBER 282 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 85 0.11873E-04 0.21001E-12 0.19983E-05 c Velocity[X] 0.10096E-12 c Velocity[Y] 0.10905E-12 c Velocity[Z] 0.20151E-37 c Pressure 0.75699E-05 5 0.51706E-08 0.61941E-05 0.25742E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062221 0.062221 9.6278e-10 9.6278e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.037e-21 5.037e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.283000000E+02 TIME STEP NUMBER 283 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 84 0.11519E-04 0.19763E-12 0.19385E-05 c Velocity[X] 0.95031E-13 c Velocity[Y] 0.10260E-12 c Velocity[Z] 0.20962E-37 c Pressure 0.73440E-05 5 0.50493E-08 0.60092E-05 0.24962E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.06222 0.06222 9.0657e-10 9.0657e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3573e-21 4.3573e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.284000000E+02 TIME STEP NUMBER 284 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 84 0.11177E-04 0.18585E-12 0.18799E-05 c Velocity[X] 0.89198E-13 c Velocity[Y] 0.96649E-13 c Velocity[Z] 0.14151E-37 c Pressure 0.71247E-05 5 0.48987E-08 0.58298E-05 0.24212E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.06222 0.06222 8.7689e-10 8.7689e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.695e-21 5.695e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.285000000E+02 TIME STEP NUMBER 285 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 83 0.10844E-04 0.17499E-12 0.18241E-05 c Velocity[X] 0.84224E-13 c Velocity[Y] 0.90769E-13 c Velocity[Z] 0.21503E-37 c Pressure 0.69121E-05 5 0.47498E-08 0.56557E-05 0.23482E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062219 0.062219 8.4689e-10 8.4689e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.1909e-21 3.1909e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.286000000E+02 TIME STEP NUMBER 286 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 82 0.10522E-04 0.16467E-12 0.17695E-05 c Velocity[X] 0.79289E-13 c Velocity[Y] 0.85384E-13 c Velocity[Z] 0.17676E-37 c Pressure 0.67058E-05 5 0.46053E-08 0.54869E-05 0.22773E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062219 0.062219 8.1793e-10 8.1793e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.9444e-21 3.9444e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.287000000E+02 TIME STEP NUMBER 287 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 82 0.10209E-04 0.15485E-12 0.17160E-05 c Velocity[X] 0.74392E-13 c Velocity[Y] 0.80458E-13 c Velocity[Z] 0.10866E-37 c Pressure 0.65056E-05 5 0.44676E-08 0.53231E-05 0.22089E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062218 0.062218 7.9126e-10 7.9126e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.4785e-21 5.4785e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.288000000E+02 TIME STEP NUMBER 288 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 81 0.99051E-05 0.14582E-12 0.16652E-05 c Velocity[X] 0.70264E-13 c Velocity[Y] 0.75554E-13 c Velocity[Z] 0.19481E-37 c Pressure 0.63114E-05 5 0.43318E-08 0.51642E-05 0.21423E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062218 0.062218 7.6435e-10 7.6435e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7482e-21 5.7482e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.289000000E+02 TIME STEP NUMBER 289 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49860E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 80 0.96104E-05 0.13723E-12 0.16154E-05 c Velocity[X] 0.66162E-13 c Velocity[Y] 0.71070E-13 c Velocity[Z] 0.14790E-37 c Pressure 0.61230E-05 5 0.42017E-08 0.50100E-05 0.20778E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062217 0.062217 7.4481e-10 7.4481e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.2916e-21 5.2916e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.290000000E+02 TIME STEP NUMBER 290 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 80 0.93245E-05 0.12902E-12 0.15663E-05 c Velocity[X] 0.62039E-13 c Velocity[Y] 0.66985E-13 c Velocity[Z] 0.23218E-37 c Pressure 0.59402E-05 5 0.40766E-08 0.48604E-05 0.20154E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062217 0.062217 7.216e-10 7.216e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.7287e-21 6.7287e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.291000000E+02 TIME STEP NUMBER 291 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 79 0.90471E-05 0.12151E-12 0.15200E-05 c Velocity[X] 0.58618E-13 c Velocity[Y] 0.62889E-13 c Velocity[Z] 0.14591E-37 c Pressure 0.57629E-05 5 0.39530E-08 0.47153E-05 0.19546E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062216 0.062216 6.9753e-10 6.9753e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7937e-21 5.7937e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8176 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.292000000E+02 TIME STEP NUMBER 292 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 78 0.87779E-05 0.11434E-12 0.14745E-05 c Velocity[X] 0.55185E-13 c Velocity[Y] 0.59158E-13 c Velocity[Z] 0.20534E-37 c Pressure 0.55909E-05 5 0.38331E-08 0.45746E-05 0.18956E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099439 1.0009 0.66381 0.66381 v Velocity[Y] -0.062216 0.062216 6.742e-10 6.742e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.325e-21 5.325e-21 v ǁVelocityǁ 0.099439 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.293000000E+02 TIME STEP NUMBER 293 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 78 0.85167E-05 0.10751E-12 0.14298E-05 c Velocity[X] 0.51735E-13 c Velocity[Y] 0.55770E-13 c Velocity[Z] 0.16055E-37 c Pressure 0.54239E-05 5 0.37191E-08 0.44380E-05 0.18387E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062215 0.062215 6.5285e-10 6.5285e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.8291e-21 4.8291e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.294000000E+02 TIME STEP NUMBER 294 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 77 0.82633E-05 0.10125E-12 0.13876E-05 c Velocity[X] 0.48904E-13 c Velocity[Y] 0.52348E-13 c Velocity[Z] 0.15881E-37 c Pressure 0.52620E-05 5 0.36064E-08 0.43055E-05 0.17832E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062215 0.062215 6.3109e-10 6.3109e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.6005e-21 6.6005e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.295000000E+02 TIME STEP NUMBER 295 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 76 0.80175E-05 0.95283E-13 0.13460E-05 c Velocity[X] 0.46040E-13 c Velocity[Y] 0.49243E-13 c Velocity[Z] 0.30801E-37 c Pressure 0.51050E-05 5 0.34971E-08 0.41769E-05 0.17294E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062215 0.062215 6.1002e-10 6.1002e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.3489e-21 6.3489e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.296000000E+02 TIME STEP NUMBER 296 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 76 0.77789E-05 0.89576E-13 0.13051E-05 c Velocity[X] 0.43141E-13 c Velocity[Y] 0.46435E-13 c Velocity[Z] 0.42688E-37 c Pressure 0.49525E-05 5 0.33933E-08 0.40522E-05 0.16775E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062214 0.062214 5.9082e-10 5.9082e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.661e-21 5.661e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.297000000E+02 TIME STEP NUMBER 297 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666989E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 75 0.75474E-05 0.84375E-13 0.12666E-05 c Velocity[X] 0.40800E-13 c Velocity[Y] 0.43574E-13 c Velocity[Z] 0.22410E-37 c Pressure 0.48047E-05 5 0.32905E-08 0.39312E-05 0.16269E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062214 0.062214 5.7115e-10 5.7115e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.4113e-21 4.4113e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.298000000E+02 TIME STEP NUMBER 298 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 75 0.73228E-05 0.79318E-13 0.12281E-05 c Velocity[X] 0.38224E-13 c Velocity[Y] 0.41094E-13 c Velocity[Z] 0.21845E-37 c Pressure 0.46612E-05 5 0.31930E-08 0.38138E-05 0.15781E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062213 0.062213 5.5325e-10 5.5325e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.9446e-21 5.9446e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.299000000E+02 TIME STEP NUMBER 299 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 74 0.71049E-05 0.74522E-13 0.11904E-05 c Velocity[X] 0.36109E-13 c Velocity[Y] 0.38412E-13 c Velocity[Z] 0.20159E-37 c Pressure 0.45221E-05 4 0.97828E-08 0.37000E-05 0.15305E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062213 0.062213 6.0607e-10 6.0607e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.3853e-21 5.3853e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.300000000E+02 TIME STEP NUMBER 300 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 73 0.68939E-05 0.70351E-13 0.11566E-05 c Velocity[X] 0.34072E-13 c Velocity[Y] 0.36279E-13 c Velocity[Z] 0.19738E-37 c Pressure 0.43870E-05 4 0.94852E-08 0.35895E-05 0.14843E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062213 0.062213 5.8258e-10 5.8258e-10 v Velocity[Z] -1.4477e-17 1.2253e-17 4.7609e-21 4.7609e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.301000000E+02 TIME STEP NUMBER 301 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 73 0.66886E-05 0.66104E-13 0.11211E-05 c Velocity[X] 0.31870E-13 c Velocity[Y] 0.34233E-13 c Velocity[Z] 0.18915E-37 c Pressure 0.42561E-05 4 0.92044E-08 0.34823E-05 0.14398E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062212 0.062212 5.6116e-10 5.6116e-10 v Velocity[Z] -1.4596e-17 1.2251e-17 2.4458e-21 2.4458e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.302000000E+02 TIME STEP NUMBER 302 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 72 0.64895E-05 0.62275E-13 0.10882E-05 c Velocity[X] 0.30169E-13 c Velocity[Y] 0.32106E-13 c Velocity[Z] 0.24131E-37 c Pressure 0.41290E-05 4 0.90417E-08 0.33783E-05 0.13962E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062212 0.062212 5.4387e-10 5.4387e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.0777e-21 7.0777e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.303000000E+02 TIME STEP NUMBER 303 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 71 0.62963E-05 0.58603E-13 0.10556E-05 c Velocity[X] 0.28402E-13 c Velocity[Y] 0.30201E-13 c Velocity[Z] 0.13644E-37 c Pressure 0.40057E-05 4 0.87614E-08 0.32775E-05 0.13539E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062212 0.062212 5.2042e-10 5.2042e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.8578e-21 5.8578e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.304000000E+02 TIME STEP NUMBER 304 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 71 0.61089E-05 0.55075E-13 0.10234E-05 c Velocity[X] 0.26575E-13 c Velocity[Y] 0.28500E-13 c Velocity[Z] 0.10446E-37 c Pressure 0.38861E-05 4 0.85041E-08 0.31796E-05 0.13133E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062212 0.062212 5.0271e-10 5.0271e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.3809e-21 6.3809e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.305000000E+02 TIME STEP NUMBER 305 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 70 0.59270E-05 0.51894E-13 0.99337E-06 c Velocity[X] 0.25171E-13 c Velocity[Y] 0.26723E-13 c Velocity[Z] 0.10054E-37 c Pressure 0.37701E-05 4 0.82485E-08 0.30847E-05 0.12737E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062211 0.062211 4.8471e-10 4.8471e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.5289e-21 4.5289e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.306000000E+02 TIME STEP NUMBER 306 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 70 0.57506E-05 0.48768E-13 0.96298E-06 c Velocity[X] 0.23545E-13 c Velocity[Y] 0.25223E-13 c Velocity[Z] 0.14804E-37 c Pressure 0.36575E-05 4 0.80063E-08 0.29925E-05 0.12356E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062211 0.062211 4.686e-10 4.686e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.0146e-21 6.0146e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.307000000E+02 TIME STEP NUMBER 307 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 69 0.55794E-05 0.45955E-13 0.93479E-06 c Velocity[X] 0.22309E-13 c Velocity[Y] 0.23646E-13 c Velocity[Z] 0.26332E-37 c Pressure 0.35483E-05 4 0.77656E-08 0.29032E-05 0.11983E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.062211 0.062211 4.5203e-10 4.5203e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.4575e-21 5.4575e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.308000000E+02 TIME STEP NUMBER 308 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666990E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 68 0.54134E-05 0.43247E-13 0.90683E-06 c Velocity[X] 0.21004E-13 c Velocity[Y] 0.22242E-13 c Velocity[Z] 0.94586E-38 c Pressure 0.34424E-05 4 0.75320E-08 0.28165E-05 0.11621E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.06221 0.06221 4.3605e-10 4.3605e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.1534e-21 5.1534e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.309000000E+02 TIME STEP NUMBER 309 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 68 0.52522E-05 0.40634E-13 0.87901E-06 c Velocity[X] 0.19630E-13 c Velocity[Y] 0.21004E-13 c Velocity[Z] 0.27888E-37 c Pressure 0.33396E-05 4 0.73114E-08 0.27324E-05 0.11274E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.06221 0.06221 4.2183e-10 4.2183e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.8675e-21 5.8675e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.310000000E+02 TIME STEP NUMBER 310 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 67 0.50959E-05 0.38297E-13 0.85336E-06 c Velocity[X] 0.18615E-13 c Velocity[Y] 0.19682E-13 c Velocity[Z] 0.13425E-37 c Pressure 0.32398E-05 4 0.70919E-08 0.26508E-05 0.10933E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.06221 0.06221 4.0703e-10 4.0703e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.6105e-21 6.6105e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.311000000E+02 TIME STEP NUMBER 311 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 67 0.49442E-05 0.35984E-13 0.82719E-06 c Velocity[X] 0.17394E-13 c Velocity[Y] 0.18590E-13 c Velocity[Z] 0.33694E-37 c Pressure 0.31431E-05 4 0.68675E-08 0.25716E-05 0.10607E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.06221 0.06221 3.9273e-10 3.9273e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.8155e-21 3.8155e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.312000000E+02 TIME STEP NUMBER 312 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 66 0.47970E-05 0.35458E-13 0.82112E-06 c Velocity[X] 0.17670E-13 c Velocity[Y] 0.17788E-13 c Velocity[Z] 0.19822E-37 c Pressure 0.30492E-05 6 0.70530E-08 0.24948E-05 0.10272E-06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099438 1.0009 0.66381 0.66381 v Velocity[Y] -0.06221 0.06221 4.279e-10 4.279e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.573e-21 5.573e-21 v ǁVelocityǁ 0.099438 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.313000000E+02 TIME STEP NUMBER 313 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 65 0.46521E-05 0.31870E-13 0.77847E-06 c Velocity[X] 0.15494E-13 c Velocity[Y] 0.16377E-13 c Velocity[Z] 0.13189E-37 c Pressure 0.29582E-05 6 0.68348E-08 0.24203E-05 0.99571E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062209 0.062209 4.1416e-10 4.1416e-10 v Velocity[Z] -1.4482e-17 1.219e-17 3.9522e-21 3.9522e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.314000000E+02 TIME STEP NUMBER 314 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 65 0.45138E-05 0.29588E-13 0.75008E-06 c Velocity[X] 0.14352E-13 c Velocity[Y] 0.15236E-13 c Velocity[Z] 0.20679E-37 c Pressure 0.28699E-05 5 0.99143E-08 0.23481E-05 0.96589E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062209 0.062209 5.6421e-10 5.6421e-10 v Velocity[Z] -1.447e-17 1.2247e-17 4.7161e-21 4.7161e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.315000000E+02 TIME STEP NUMBER 315 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 64 0.43815E-05 0.28229E-13 0.73265E-06 c Velocity[X] 0.13761E-13 c Velocity[Y] 0.14468E-13 c Velocity[Z] 0.24890E-37 c Pressure 0.27843E-05 5 0.96170E-08 0.22781E-05 0.93671E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062209 0.062209 5.4966e-10 5.4966e-10 v Velocity[Z] -1.4481e-17 1.2249e-17 4.7827e-21 4.7827e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.316000000E+02 TIME STEP NUMBER 316 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 64 0.42508E-05 0.26514E-13 0.71005E-06 c Velocity[X] 0.12802E-13 c Velocity[Y] 0.13712E-13 c Velocity[Z] 0.81361E-38 c Pressure 0.27011E-05 5 0.93294E-08 0.22100E-05 0.90878E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062209 0.062209 5.3286e-10 5.3286e-10 v Velocity[Z] -1.4471e-17 1.2252e-17 5.2939e-21 5.2939e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.317000000E+02 TIME STEP NUMBER 317 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666991E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 63 0.41241E-05 0.25011E-13 0.68962E-06 c Velocity[X] 0.12171E-13 c Velocity[Y] 0.12840E-13 c Velocity[Z] 0.12925E-37 c Pressure 0.26205E-05 5 0.90471E-08 0.21440E-05 0.88127E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062208 0.062208 5.1454e-10 5.1454e-10 v Velocity[Z] -1.4514e-17 1.2252e-17 5.569e-21 5.569e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.318000000E+02 TIME STEP NUMBER 318 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 62 0.40011E-05 0.23527E-13 0.66885E-06 c Velocity[X] 0.11452E-13 c Velocity[Y] 0.12075E-13 c Velocity[Z] 0.16504E-37 c Pressure 0.25422E-05 5 0.87739E-08 0.20800E-05 0.85469E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062208 0.062208 4.9471e-10 4.9471e-10 v Velocity[Z] -1.4481e-17 1.2157e-17 5.0234e-21 5.0234e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.319000000E+02 TIME STEP NUMBER 319 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 62 0.38819E-05 0.22091E-13 0.64812E-06 c Velocity[X] 0.10670E-13 c Velocity[Y] 0.11421E-13 c Velocity[Z] 0.14614E-37 c Pressure 0.24663E-05 5 0.85122E-08 0.20178E-05 0.82921E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062208 0.062208 4.7889e-10 4.7889e-10 v Velocity[Z] -1.4471e-17 1.2249e-17 4.6067e-21 4.6067e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.320000000E+02 TIME STEP NUMBER 320 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 61 0.37662E-05 0.20834E-13 0.62942E-06 c Velocity[X] 0.10150E-13 c Velocity[Y] 0.10684E-13 c Velocity[Z] 0.95947E-38 c Pressure 0.23926E-05 5 0.82553E-08 0.19576E-05 0.80421E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062208 0.062208 4.6128e-10 4.6128e-10 v Velocity[Z] -1.4598e-17 1.2251e-17 5.0244e-21 5.0244e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.321000000E+02 TIME STEP NUMBER 321 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 61 0.36541E-05 0.19561E-13 0.60988E-06 c Velocity[X] 0.94530E-14 c Velocity[Y] 0.10108E-13 c Velocity[Z] 0.13856E-37 c Pressure 0.23211E-05 5 0.80092E-08 0.18991E-05 0.78025E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062208 0.062208 4.4689e-10 4.4689e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.1838e-21 7.1838e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.322000000E+02 TIME STEP NUMBER 322 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 60 0.35452E-05 0.18451E-13 0.59232E-06 c Velocity[X] 0.89986E-14 c Velocity[Y] 0.94525E-14 c Velocity[Z] 0.17206E-37 c Pressure 0.22518E-05 5 0.77675E-08 0.18424E-05 0.75672E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062208 0.062208 4.3068e-10 4.3068e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.8012e-21 3.8012e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.323000000E+02 TIME STEP NUMBER 323 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 60 0.34396E-05 0.17321E-13 0.57390E-06 c Velocity[X] 0.83750E-14 c Velocity[Y] 0.89461E-14 c Velocity[Z] 0.13245E-37 c Pressure 0.21845E-05 5 0.75362E-08 0.17873E-05 0.73418E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062207 0.062207 4.1758e-10 4.1758e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3434e-21 4.3434e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.324000000E+02 TIME STEP NUMBER 324 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 59 0.33371E-05 0.16341E-13 0.55742E-06 c Velocity[X] 0.79779E-14 c Velocity[Y] 0.83627E-14 c Velocity[Z] 0.21666E-37 c Pressure 0.21193E-05 5 0.73087E-08 0.17339E-05 0.71203E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062207 0.062207 4.0262e-10 4.0262e-10 v Velocity[Z] -1.4597e-17 1.2251e-17 8.7825e-21 8.7825e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.325000000E+02 TIME STEP NUMBER 325 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 59 0.32378E-05 0.15338E-13 0.54004E-06 c Velocity[X] 0.74196E-14 c Velocity[Y] 0.79179E-14 c Velocity[Z] 0.34409E-37 c Pressure 0.20560E-05 5 0.70912E-08 0.16821E-05 0.69083E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062207 0.062207 3.9062e-10 3.9062e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.858e-21 4.858e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.326000000E+02 TIME STEP NUMBER 326 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93278E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 58 0.31413E-05 0.14472E-13 0.52458E-06 c Velocity[X] 0.70732E-14 c Velocity[Y] 0.73986E-14 c Velocity[Z] 0.16315E-37 c Pressure 0.19946E-05 5 0.68772E-08 0.16319E-05 0.66998E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062207 0.062207 3.7675e-10 3.7675e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.5702e-21 4.5702e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.327000000E+02 TIME STEP NUMBER 327 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 57 0.30477E-05 0.13620E-13 0.50891E-06 c Velocity[X] 0.66616E-14 c Velocity[Y] 0.69587E-14 c Velocity[Z] 0.22836E-37 c Pressure 0.19350E-05 5 0.66695E-08 0.15831E-05 0.64975E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062207 0.062207 3.633e-10 3.633e-10 v Velocity[Z] -1.4597e-17 1.2251e-17 6.4265e-21 6.4265e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.328000000E+02 TIME STEP NUMBER 328 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 57 0.29570E-05 0.12392E-13 0.48542E-06 c Velocity[X] 0.60049E-14 c Velocity[Y] 0.63870E-14 c Velocity[Z] 0.12961E-37 c Pressure 0.18772E-05 4 0.99799E-08 0.15358E-05 0.63041E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062207 0.062207 4.9044e-10 4.9044e-10 v Velocity[Z] -1.4597e-17 1.2251e-17 7.7276e-21 7.7276e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.329000000E+02 TIME STEP NUMBER 329 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 56 0.28696E-05 0.12110E-13 0.47986E-06 c Velocity[X] 0.59409E-14 c Velocity[Y] 0.61689E-14 c Velocity[Z] 0.16761E-37 c Pressure 0.18213E-05 4 0.96781E-08 0.14901E-05 0.61100E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062207 0.062207 4.7099e-10 4.7099e-10 v Velocity[Z] -1.4479e-17 1.2217e-17 6.2575e-21 6.2575e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.330000000E+02 TIME STEP NUMBER 330 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 56 0.27843E-05 0.11340E-13 0.46436E-06 c Velocity[X] 0.54894E-14 c Velocity[Y] 0.58506E-14 c Velocity[Z] 0.13955E-37 c Pressure 0.17669E-05 4 0.93931E-08 0.14456E-05 0.59287E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062206 0.062206 4.5633e-10 4.5633e-10 v Velocity[Z] -1.4542e-17 1.225e-17 6.882e-21 6.882e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.331000000E+02 TIME STEP NUMBER 331 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 55 0.27015E-05 0.10705E-13 0.45117E-06 c Velocity[X] 0.52463E-14 c Velocity[Y] 0.54587E-14 c Velocity[Z] 0.32023E-37 c Pressure 0.17140E-05 4 0.91121E-08 0.14024E-05 0.57497E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062206 0.062206 4.3972e-10 4.3972e-10 v Velocity[Z] -1.4597e-17 1.2251e-17 3.7759e-21 3.7759e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.332000000E+02 TIME STEP NUMBER 332 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 55 0.26211E-05 0.10040E-13 0.43693E-06 c Velocity[X] 0.48617E-14 c Velocity[Y] 0.51779E-14 c Velocity[Z] 0.17113E-37 c Pressure 0.16628E-05 4 0.88423E-08 0.13604E-05 0.55789E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062206 0.062206 4.2612e-10 4.2612e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.1987e-21 5.1987e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.333000000E+02 TIME STEP NUMBER 333 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 54 0.25431E-05 0.94804E-14 0.42458E-06 c Velocity[X] 0.46511E-14 c Velocity[Y] 0.48293E-14 c Velocity[Z] 0.12620E-37 c Pressure 0.16131E-05 4 0.85769E-08 0.13197E-05 0.54104E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062206 0.062206 4.1017e-10 4.1017e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.505e-21 4.505e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.334000000E+02 TIME STEP NUMBER 334 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 54 0.24674E-05 0.88905E-14 0.41116E-06 c Velocity[X] 0.43069E-14 c Velocity[Y] 0.45836E-14 c Velocity[Z] 0.19186E-37 c Pressure 0.15648E-05 4 0.83214E-08 0.12803E-05 0.52475E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062206 0.062206 3.9885e-10 3.9885e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.8882e-21 3.8882e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.335000000E+02 TIME STEP NUMBER 335 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 53 0.23939E-05 0.83963E-14 0.39957E-06 c Velocity[X] 0.41235E-14 c Velocity[Y] 0.42728E-14 c Velocity[Z] 0.15450E-37 c Pressure 0.15180E-05 4 0.80712E-08 0.12420E-05 0.50892E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062206 0.062206 3.8343e-10 3.8343e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.502e-21 4.502e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.336000000E+02 TIME STEP NUMBER 336 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 53 0.23226E-05 0.78710E-14 0.38687E-06 c Velocity[X] 0.38133E-14 c Velocity[Y] 0.40578E-14 c Velocity[Z] 0.12949E-37 c Pressure 0.14726E-05 4 0.78319E-08 0.12048E-05 0.49382E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062206 0.062206 3.7088e-10 3.7088e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7817e-21 5.7817e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.337000000E+02 TIME STEP NUMBER 337 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 52 0.22534E-05 0.74363E-14 0.37604E-06 c Velocity[X] 0.36572E-14 c Velocity[Y] 0.37791E-14 c Velocity[Z] 0.82804E-38 c Pressure 0.14286E-05 4 0.75963E-08 0.11688E-05 0.47889E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062206 0.062206 3.5791e-10 3.5791e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.9216e-21 6.9216e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.338000000E+02 TIME STEP NUMBER 338 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 52 0.21863E-05 0.69694E-14 0.36404E-06 c Velocity[X] 0.33772E-14 c Velocity[Y] 0.35921E-14 c Velocity[Z] 0.30018E-37 c Pressure 0.13859E-05 4 0.73711E-08 0.11339E-05 0.46468E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 3.46e-10 3.46e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.1084e-21 4.1084e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.339000000E+02 TIME STEP NUMBER 339 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 51 0.21211E-05 0.65863E-14 0.35389E-06 c Velocity[X] 0.32423E-14 c Velocity[Y] 0.33441E-14 c Velocity[Z] 0.19340E-37 c Pressure 0.13444E-05 4 0.71491E-08 0.11000E-05 0.45062E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 3.3215e-10 3.3215e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.686e-21 5.686e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.340000000E+02 TIME STEP NUMBER 340 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 51 0.20579E-05 0.61708E-14 0.34255E-06 c Velocity[X] 0.29907E-14 c Velocity[Y] 0.31801E-14 c Velocity[Z] 0.29227E-37 c Pressure 0.13042E-05 4 0.69372E-08 0.10671E-05 0.43726E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 3.2112e-10 3.2112e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.1083e-21 7.1083e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.341000000E+02 TIME STEP NUMBER 341 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 50 0.19966E-05 0.58335E-14 0.33305E-06 c Velocity[X] 0.28752E-14 c Velocity[Y] 0.29582E-14 c Velocity[Z] 0.25600E-37 c Pressure 0.12652E-05 4 0.67282E-08 0.10352E-05 0.42402E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 3.081e-10 3.081e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.9817e-21 3.9817e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.342000000E+02 TIME STEP NUMBER 342 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 50 0.19371E-05 0.54638E-14 0.32233E-06 c Velocity[X] 0.26484E-14 c Velocity[Y] 0.28153E-14 c Velocity[Z] 0.16628E-37 c Pressure 0.12274E-05 4 0.65288E-08 0.10042E-05 0.41145E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 2.9787e-10 2.9787e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.4776e-21 4.4776e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.343000000E+02 TIME STEP NUMBER 343 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 49 0.18793E-05 0.51667E-14 0.31344E-06 c Velocity[X] 0.25499E-14 c Velocity[Y] 0.26169E-14 c Velocity[Z] 0.25562E-37 c Pressure 0.11907E-05 4 0.63319E-08 0.97418E-06 0.39899E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 2.857e-10 2.857e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.584e-21 4.584e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.344000000E+02 TIME STEP NUMBER 344 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 49 0.18233E-05 0.48377E-14 0.30330E-06 c Velocity[X] 0.23452E-14 c Velocity[Y] 0.24925E-14 c Velocity[Z] 0.19626E-37 c Pressure 0.11551E-05 4 0.61443E-08 0.94503E-06 0.38717E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 2.7626e-10 2.7626e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.4302e-21 7.4302e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.345000000E+02 TIME STEP NUMBER 345 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 48 0.17689E-05 0.45762E-14 0.29499E-06 c Velocity[X] 0.22615E-14 c Velocity[Y] 0.23148E-14 c Velocity[Z] 0.19109E-37 c Pressure 0.11206E-05 4 0.59589E-08 0.91679E-06 0.37543E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 2.6492e-10 2.6492e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3937e-21 4.3937e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.346000000E+02 TIME STEP NUMBER 346 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 48 0.17162E-05 0.42833E-14 0.28539E-06 c Velocity[X] 0.20766E-14 c Velocity[Y] 0.22067E-14 c Velocity[Z] 0.14132E-37 c Pressure 0.10870E-05 4 0.57825E-08 0.88936E-06 0.36432E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 2.5624e-10 2.5624e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7576e-21 5.7576e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.347000000E+02 TIME STEP NUMBER 347 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 47 0.16650E-05 0.40533E-14 0.27762E-06 c Velocity[X] 0.20058E-14 c Velocity[Y] 0.20475E-14 c Velocity[Z] 0.12570E-37 c Pressure 0.10545E-05 4 0.56078E-08 0.86278E-06 0.35327E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 2.4569e-10 2.4569e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.0771e-21 5.0771e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.348000000E+02 TIME STEP NUMBER 348 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 47 0.16154E-05 0.37923E-14 0.26854E-06 c Velocity[X] 0.18386E-14 c Velocity[Y] 0.19538E-14 c Velocity[Z] 0.16455E-37 c Pressure 0.10230E-05 4 0.54419E-08 0.83697E-06 0.34282E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 2.3773e-10 2.3773e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.6404e-21 6.6404e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.349000000E+02 TIME STEP NUMBER 349 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 46 0.15672E-05 0.35922E-14 0.26135E-06 c Velocity[X] 0.17649E-14 c Velocity[Y] 0.18273E-14 c Velocity[Z] 0.23787E-37 c Pressure 0.99242E-06 3 0.97024E-08 0.81195E-06 0.33240E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062205 0.062205 2.5508e-10 2.5508e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.0868e-21 4.0868e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.350000000E+02 TIME STEP NUMBER 350 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 46 0.15208E-05 0.33624E-14 0.25286E-06 c Velocity[X] 0.16301E-14 c Velocity[Y] 0.17323E-14 c Velocity[Z] 0.17816E-37 c Pressure 0.96289E-06 3 0.94403E-08 0.78779E-06 0.32257E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 2.4924e-10 2.4924e-10 v Velocity[Z] -1.4476e-17 1.2245e-17 7.4703e-21 7.4703e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.351000000E+02 TIME STEP NUMBER 351 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 45 0.14754E-05 0.31816E-14 0.24597E-06 c Velocity[X] 0.15820E-14 c Velocity[Y] 0.15996E-14 c Velocity[Z] 0.11951E-37 c Pressure 0.93409E-06 3 0.91621E-08 0.76422E-06 0.31277E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 2.4135e-10 2.4135e-10 v Velocity[Z] -1.4596e-17 1.225e-17 5.6502e-21 5.6502e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.352000000E+02 TIME STEP NUMBER 352 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 45 0.14315E-05 0.29738E-14 0.23780E-06 c Velocity[X] 0.14437E-14 c Velocity[Y] 0.15301E-14 c Velocity[Z] 0.12764E-37 c Pressure 0.90612E-06 3 0.88932E-08 0.74134E-06 0.30353E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099437 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 2.3531e-10 2.3531e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5845e-21 5.5845e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.353000000E+02 TIME STEP NUMBER 353 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 44 0.13888E-05 0.28181E-14 0.23149E-06 c Velocity[X] 0.14025E-14 c Velocity[Y] 0.14156E-14 c Velocity[Z] 0.14573E-37 c Pressure 0.87902E-06 3 0.86274E-08 0.71916E-06 0.29430E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 2.2675e-10 2.2675e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.7339e-21 3.7339e-21 v ǁVelocityǁ 0.099437 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.354000000E+02 TIME STEP NUMBER 354 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 44 0.13474E-05 0.26329E-14 0.22375E-06 c Velocity[X] 0.12774E-14 c Velocity[Y] 0.13555E-14 c Velocity[Z] 0.22252E-37 c Pressure 0.85271E-06 3 0.83737E-08 0.69764E-06 0.28562E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 2.2034e-10 2.2034e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.5286e-21 7.5286e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.355000000E+02 TIME STEP NUMBER 355 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 43 0.13072E-05 0.24964E-14 0.21788E-06 c Velocity[X] 0.12441E-14 c Velocity[Y] 0.12524E-14 c Velocity[Z] 0.11339E-37 c Pressure 0.82720E-06 3 0.81232E-08 0.67677E-06 0.27692E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 2.1172e-10 2.1172e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.3281e-21 7.3281e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.356000000E+02 TIME STEP NUMBER 356 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 43 0.12682E-05 0.23311E-14 0.21054E-06 c Velocity[X] 0.11305E-14 c Velocity[Y] 0.12007E-14 c Velocity[Z] 0.13527E-37 c Pressure 0.80244E-06 3 0.78845E-08 0.65651E-06 0.26876E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 2.054e-10 2.054e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5233e-21 5.5233e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.357000000E+02 TIME STEP NUMBER 357 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 42 0.12304E-05 0.22115E-14 0.20507E-06 c Velocity[X] 0.11038E-14 c Velocity[Y] 0.11077E-14 c Velocity[Z] 0.10033E-37 c Pressure 0.77844E-06 3 0.76486E-08 0.63688E-06 0.26056E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.9704e-10 1.9704e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.675e-21 4.675e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.358000000E+02 TIME STEP NUMBER 358 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 42 0.11937E-05 0.20648E-14 0.19815E-06 c Velocity[X] 0.10020E-14 c Velocity[Y] 0.10628E-14 c Velocity[Z] 0.18258E-37 c Pressure 0.75514E-06 3 0.74380E-08 0.61782E-06 0.25264E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.9782e-10 1.9782e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.77e-21 4.77e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.359000000E+02 TIME STEP NUMBER 359 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 41 0.11580E-05 0.19591E-14 0.19301E-06 c Velocity[X] 0.97923E-15 c Velocity[Y] 0.97988E-15 c Velocity[Z] 0.14142E-37 c Pressure 0.73256E-06 3 0.72181E-08 0.59934E-06 0.24496E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.9022e-10 1.9022e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.8775e-21 7.8775e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.360000000E+02 TIME STEP NUMBER 360 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 41 0.11235E-05 0.18271E-14 0.18639E-06 c Velocity[X] 0.88517E-15 c Velocity[Y] 0.94195E-15 c Velocity[Z] 0.29785E-37 c Pressure 0.71063E-06 3 0.70080E-08 0.58140E-06 0.23776E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.8445e-10 1.8445e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.393e-21 3.393e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.361000000E+02 TIME STEP NUMBER 361 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 41 0.10900E-05 0.17191E-14 0.18080E-06 c Velocity[X] 0.83286E-15 c Velocity[Y] 0.88624E-15 c Velocity[Z] 0.25689E-37 c Pressure 0.68937E-06 3 0.68040E-08 0.56400E-06 0.23078E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.7893e-10 1.7893e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.5667e-21 6.5667e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.362000000E+02 TIME STEP NUMBER 362 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 40 0.10575E-05 0.16335E-14 0.17624E-06 c Velocity[X] 0.81876E-15 c Velocity[Y] 0.81469E-15 c Velocity[Z] 0.10189E-37 c Pressure 0.66875E-06 3 0.66013E-08 0.54713E-06 0.22372E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.7148e-10 1.7148e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.5915e-21 6.5915e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.363000000E+02 TIME STEP NUMBER 363 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 40 0.10259E-05 0.15222E-14 0.17013E-06 c Velocity[X] 0.73766E-15 c Velocity[Y] 0.78455E-15 c Velocity[Z] 0.24290E-37 c Pressure 0.64873E-06 3 0.64093E-08 0.53076E-06 0.21715E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.6624e-10 1.6624e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5952e-21 5.5952e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.364000000E+02 TIME STEP NUMBER 364 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 39 0.99529E-06 0.14472E-14 0.16589E-06 c Velocity[X] 0.72683E-15 c Velocity[Y] 0.72035E-15 c Velocity[Z] 0.19130E-37 c Pressure 0.62933E-06 3 0.62185E-08 0.51488E-06 0.21050E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.5924e-10 1.5924e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.5989e-21 3.5989e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.365000000E+02 TIME STEP NUMBER 365 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 39 0.96562E-06 0.13475E-14 0.16007E-06 c Velocity[X] 0.65261E-15 c Velocity[Y] 0.69493E-15 c Velocity[Z] 0.16194E-37 c Pressure 0.61049E-06 3 0.60380E-08 0.49947E-06 0.20433E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.5443e-10 1.5443e-10 v Velocity[Z] -1.4597e-17 1.225e-17 1.6291e-21 1.6291e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.366000000E+02 TIME STEP NUMBER 366 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 38 0.93675E-06 0.12822E-14 0.15615E-06 c Velocity[X] 0.64533E-15 c Velocity[Y] 0.63687E-15 c Velocity[Z] 0.16136E-37 c Pressure 0.59223E-06 3 0.58584E-08 0.48452E-06 0.19806E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.4788e-10 1.4788e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.5318e-21 3.5318e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.367000000E+02 TIME STEP NUMBER 367 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 38 0.90883E-06 0.11929E-14 0.15061E-06 c Velocity[X] 0.57788E-15 c Velocity[Y] 0.61502E-15 c Velocity[Z] 0.23274E-37 c Pressure 0.57450E-06 3 0.57080E-08 0.47002E-06 0.19211E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062204 0.062204 1.4728e-10 1.4728e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.8346e-21 6.8346e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.368000000E+02 TIME STEP NUMBER 368 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 37 0.88164E-06 0.11360E-14 0.14697E-06 c Velocity[X] 0.57294E-15 c Velocity[Y] 0.56305E-15 c Velocity[Z] 0.77400E-38 c Pressure 0.55731E-06 3 0.55419E-08 0.45596E-06 0.18622E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.4154e-10 1.4154e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.1878e-21 6.1878e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.369000000E+02 TIME STEP NUMBER 369 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 37 0.85536E-06 0.10559E-14 0.14170E-06 c Velocity[X] 0.51057E-15 c Velocity[Y] 0.54531E-15 c Velocity[Z] 0.17349E-37 c Pressure 0.54063E-06 3 0.53840E-08 0.44231E-06 0.18077E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.3755e-10 1.3755e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.1454e-21 7.1454e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.370000000E+02 TIME STEP NUMBER 370 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 37 0.82987E-06 0.99335E-15 0.13744E-06 c Velocity[X] 0.48022E-15 c Velocity[Y] 0.51313E-15 c Velocity[Z] 0.23536E-37 c Pressure 0.52445E-06 3 0.52306E-08 0.42908E-06 0.17549E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.3379e-10 1.3379e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.6445e-21 3.6445e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.371000000E+02 TIME STEP NUMBER 371 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 36 0.80504E-06 0.94740E-15 0.13422E-06 c Velocity[X] 0.47950E-15 c Velocity[Y] 0.46790E-15 c Velocity[Z] 0.30013E-37 c Pressure 0.50875E-06 3 0.50766E-08 0.41623E-06 0.17009E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.2822e-10 1.2822e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.9067e-21 3.9067e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.372000000E+02 TIME STEP NUMBER 372 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 36 0.78105E-06 0.87956E-15 0.12932E-06 c Velocity[X] 0.42533E-15 c Velocity[Y] 0.45423E-15 c Velocity[Z] 0.22335E-37 c Pressure 0.49353E-06 3 0.49321E-08 0.40378E-06 0.16512E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.2466e-10 1.2466e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.158e-21 6.158e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.373000000E+02 TIME STEP NUMBER 373 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 35 0.75767E-06 0.83957E-15 0.12635E-06 c Velocity[X] 0.42604E-15 c Velocity[Y] 0.41353E-15 c Velocity[Z] 0.21867E-37 c Pressure 0.47875E-06 3 0.47870E-08 0.39169E-06 0.16002E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.1944e-10 1.1944e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.4845e-21 4.4845e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.374000000E+02 TIME STEP NUMBER 374 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 35 0.73508E-06 0.90991E-15 0.13154E-06 c Velocity[X] 0.39327E-15 c Velocity[Y] 0.51664E-15 c Velocity[Z] 0.13386E-37 c Pressure 0.46443E-06 5 0.62267E-08 0.37997E-06 0.15571E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.2082e-10 1.2082e-10 v Velocity[Z] -1.4597e-17 1.225e-17 2.3541e-21 2.3541e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.375000000E+02 TIME STEP NUMBER 375 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 375, Physical time 0.37500E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 375: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 35 0.71240E-06 0.73239E-15 0.11801E-06 c Velocity[X] 0.35454E-15 c Velocity[Y] 0.37785E-15 c Velocity[Z] 0.23857E-37 c Pressure 0.45044E-06 5 0.60540E-08 0.36852E-06 0.15119E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.2126e-10 1.2126e-10 v Velocity[Z] -1.4482e-17 1.2251e-17 4.6175e-21 4.6175e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.376000000E+02 TIME STEP NUMBER 376 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 34 0.69108E-06 0.80095E-15 0.12341E-06 c Velocity[X] 0.35374E-15 c Velocity[Y] 0.44721E-15 c Velocity[Z] 0.20124E-37 c Pressure 0.43699E-06 4 0.99103E-08 0.35752E-06 0.14648E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.0273e-10 2.0273e-10 v Velocity[Z] -1.4596e-17 1.2251e-17 6.658e-21 6.658e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.377000000E+02 TIME STEP NUMBER 377 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 34 0.67025E-06 0.64936E-15 0.11112E-06 c Velocity[X] 0.31736E-15 c Velocity[Y] 0.33201E-15 c Velocity[Z] 0.12494E-37 c Pressure 0.42406E-06 4 0.96202E-08 0.34694E-06 0.14217E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.012e-10 2.012e-10 v Velocity[Z] -1.4474e-17 1.225e-17 6.456e-21 6.456e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.378000000E+02 TIME STEP NUMBER 378 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 33 0.65030E-06 0.61716E-15 0.10833E-06 c Velocity[X] 0.32232E-15 c Velocity[Y] 0.29484E-15 c Velocity[Z] 0.26361E-37 c Pressure 0.41141E-06 4 0.93281E-08 0.33659E-06 0.13772E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.9178e-10 1.9178e-10 v Velocity[Z] -1.4596e-17 1.225e-17 6.9326e-21 6.9326e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.379000000E+02 TIME STEP NUMBER 379 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 33 0.63106E-06 0.57024E-15 0.10413E-06 c Velocity[X] 0.28107E-15 c Velocity[Y] 0.28918E-15 c Velocity[Z] 0.97507E-38 c Pressure 0.39914E-06 4 0.90531E-08 0.32655E-06 0.13369E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.8719e-10 1.8719e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7566e-21 5.7566e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.380000000E+02 TIME STEP NUMBER 380 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 33 0.61239E-06 0.53630E-15 0.10098E-06 c Velocity[X] 0.26393E-15 c Velocity[Y] 0.27237E-15 c Velocity[Z] 0.21286E-37 c Pressure 0.38722E-06 4 0.87866E-08 0.31680E-06 0.12979E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.8341e-10 1.8341e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.4676e-21 3.4676e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.381000000E+02 TIME STEP NUMBER 381 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 32 0.59411E-06 0.51442E-15 0.98903E-07 c Velocity[X] 0.26933E-15 c Velocity[Y] 0.24509E-15 c Velocity[Z] 0.15787E-37 c Pressure 0.37563E-06 4 0.85192E-08 0.30732E-06 0.12572E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.7549e-10 1.7549e-10 v Velocity[Z] -1.4597e-17 1.225e-17 2.069e-21 2.069e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.382000000E+02 TIME STEP NUMBER 382 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 32 0.57649E-06 0.47487E-15 0.95025E-07 c Velocity[X] 0.23346E-15 c Velocity[Y] 0.24142E-15 c Velocity[Z] 0.19497E-37 c Pressure 0.36442E-06 4 0.82687E-08 0.29814E-06 0.12205E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.7206e-10 1.7206e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.7869e-21 4.7869e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.383000000E+02 TIME STEP NUMBER 383 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 31 0.55923E-06 0.45611E-15 0.93129E-07 c Velocity[X] 0.23932E-15 c Velocity[Y] 0.21680E-15 c Velocity[Z] 0.21162E-37 c Pressure 0.35350E-06 4 0.80167E-08 0.28921E-06 0.11821E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.6477e-10 1.6477e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.1595e-21 6.1595e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.384000000E+02 TIME STEP NUMBER 384 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 31 0.54263E-06 0.42031E-15 0.89400E-07 c Velocity[X] 0.20602E-15 c Velocity[Y] 0.21430E-15 c Velocity[Z] 0.18589E-37 c Pressure 0.34295E-06 4 0.77813E-08 0.28058E-06 0.11477E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.6185e-10 1.6185e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.3692e-21 6.3692e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.385000000E+02 TIME STEP NUMBER 385 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 31 0.52652E-06 0.39537E-15 0.86706E-07 c Velocity[X] 0.19344E-15 c Velocity[Y] 0.20192E-15 c Velocity[Z] 0.15876E-37 c Pressure 0.33271E-06 4 0.75530E-08 0.27220E-06 0.11144E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.5942e-10 1.5942e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3402e-21 4.3402e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.386000000E+02 TIME STEP NUMBER 386 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 30 0.51072E-06 0.38075E-15 0.85089E-07 c Velocity[X] 0.20042E-15 c Velocity[Y] 0.18033E-15 c Velocity[Z] 0.15338E-37 c Pressure 0.32274E-06 4 0.73224E-08 0.26404E-06 0.10792E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.528e-10 1.528e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.2133e-21 5.2133e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.387000000E+02 TIME STEP NUMBER 387 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 30 0.49555E-06 0.35015E-15 0.81597E-07 c Velocity[X] 0.17122E-15 c Velocity[Y] 0.17893E-15 c Velocity[Z] 0.22958E-37 c Pressure 0.31310E-06 4 0.71077E-08 0.25616E-06 0.10479E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.5028e-10 1.5028e-10 v Velocity[Z] -1.4597e-17 1.225e-17 2.9314e-21 2.9314e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.388000000E+02 TIME STEP NUMBER 388 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 29 0.48065E-06 0.44353E-15 0.91836E-07 c Velocity[X] 0.18777E-15 c Velocity[Y] 0.25576E-15 c Velocity[Z] 0.20514E-37 c Pressure 0.30370E-06 3 0.97737E-08 0.24847E-06 0.10146E-07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.55e-10 2.55e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.6052e-21 4.6052e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.389000000E+02 TIME STEP NUMBER 389 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 29 0.46842E-06 0.32009E-15 0.78017E-07 c Velocity[X] 0.15931E-15 c Velocity[Y] 0.16079E-15 c Velocity[Z] 0.89767E-38 c Pressure 0.29465E-06 3 0.94528E-08 0.24106E-06 0.98453E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.4747e-10 2.4747e-10 v Velocity[Z] -1.4474e-17 1.225e-17 4.5179e-21 4.5179e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.390000000E+02 TIME STEP NUMBER 390 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 29 0.45428E-06 0.29222E-15 0.74543E-07 c Velocity[X] 0.14450E-15 c Velocity[Y] 0.14772E-15 c Velocity[Z] 0.17500E-37 c Pressure 0.28588E-06 3 0.91875E-08 0.23389E-06 0.95613E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.4156e-10 2.4156e-10 v Velocity[Z] -1.4596e-17 1.225e-17 4.2959e-21 4.2959e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.391000000E+02 TIME STEP NUMBER 391 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 28 0.44043E-06 0.28206E-15 0.73235E-07 c Velocity[X] 0.15149E-15 c Velocity[Y] 0.13057E-15 c Velocity[Z] 0.21191E-37 c Pressure 0.27728E-06 3 0.89175E-08 0.22685E-06 0.92571E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.3035e-10 2.3035e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.9538e-21 5.9538e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.392000000E+02 TIME STEP NUMBER 392 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 28 0.42721E-06 0.25813E-15 0.70060E-07 c Velocity[X] 0.12712E-15 c Velocity[Y] 0.13100E-15 c Velocity[Z] 0.23751E-37 c Pressure 0.26900E-06 3 0.86652E-08 0.22008E-06 0.89900E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.2314e-10 2.2314e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.6053e-21 3.6053e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.393000000E+02 TIME STEP NUMBER 393 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 28 0.41441E-06 0.24269E-15 0.67932E-07 c Velocity[X] 0.11914E-15 c Velocity[Y] 0.12355E-15 c Velocity[Z] 0.15219E-37 c Pressure 0.26097E-06 3 0.84190E-08 0.21351E-06 0.87316E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.1633e-10 2.1633e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3136e-21 4.3136e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.394000000E+02 TIME STEP NUMBER 394 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 27 0.40178E-06 0.23540E-15 0.66905E-07 c Velocity[X] 0.12682E-15 c Velocity[Y] 0.10859E-15 c Velocity[Z] 0.14240E-37 c Pressure 0.25311E-06 3 0.81667E-08 0.20708E-06 0.84523E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 2.051e-10 2.051e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.6481e-21 6.6481e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.395000000E+02 TIME STEP NUMBER 395 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 27 0.38975E-06 0.21486E-15 0.63918E-07 c Velocity[X] 0.10540E-15 c Velocity[Y] 0.10946E-15 c Velocity[Z] 0.20258E-37 c Pressure 0.24556E-06 3 0.79329E-08 0.20090E-06 0.82090E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.9818e-10 1.9818e-10 v Velocity[Z] -1.4597e-17 1.225e-17 2.7667e-21 2.7667e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.396000000E+02 TIME STEP NUMBER 396 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 27 0.37809E-06 0.20203E-15 0.61980E-07 c Velocity[X] 0.98779E-16 c Velocity[Y] 0.10325E-15 c Velocity[Z] 0.25750E-37 c Pressure 0.23823E-06 3 0.77053E-08 0.19490E-06 0.79737E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.9193e-10 1.9193e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.8269e-21 5.8269e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.397000000E+02 TIME STEP NUMBER 397 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666992E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 26 0.36656E-06 0.19667E-15 0.61152E-07 c Velocity[X] 0.10645E-15 c Velocity[Y] 0.90216E-16 c Velocity[Z] 0.84389E-38 c Pressure 0.23104E-06 3 0.74716E-08 0.18902E-06 0.77170E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.8155e-10 1.8155e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.0935e-21 6.0935e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.398000000E+02 TIME STEP NUMBER 398 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 26 0.35560E-06 0.17888E-15 0.58322E-07 c Velocity[X] 0.87452E-16 c Velocity[Y] 0.91432E-16 c Velocity[Z] 0.88733E-38 c Pressure 0.22415E-06 3 0.72564E-08 0.18338E-06 0.74956E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.7545e-10 1.7545e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.6995e-21 4.6995e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.399000000E+02 TIME STEP NUMBER 399 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 26 0.34498E-06 0.16819E-15 0.56553E-07 c Velocity[X] 0.81917E-16 c Velocity[Y] 0.86275E-16 c Velocity[Z] 0.17602E-37 c Pressure 0.21746E-06 3 0.70473E-08 0.17791E-06 0.72815E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.7007e-10 1.7007e-10 v Velocity[Z] -1.4597e-17 1.225e-17 2.7806e-21 2.7806e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.400000000E+02 TIME STEP NUMBER 400 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 25 0.33443E-06 0.16439E-15 0.55910E-07 c Velocity[X] 0.89473E-16 c Velocity[Y] 0.74918E-16 c Velocity[Z] 0.11390E-37 c Pressure 0.21088E-06 3 0.68314E-08 0.17253E-06 0.70454E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.6069e-10 1.6069e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7229e-21 5.7229e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.401000000E+02 TIME STEP NUMBER 401 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 25 0.32444E-06 0.14893E-15 0.53216E-07 c Velocity[X] 0.72555E-16 c Velocity[Y] 0.76373E-16 c Velocity[Z] 0.10888E-37 c Pressure 0.20459E-06 3 0.66342E-08 0.16738E-06 0.68439E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.5547e-10 1.5547e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.9738e-21 5.9738e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.402000000E+02 TIME STEP NUMBER 402 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 25 0.31476E-06 0.14001E-15 0.51598E-07 c Velocity[X] 0.67914E-16 c Velocity[Y] 0.72098E-16 c Velocity[Z] 0.71174E-38 c Pressure 0.19849E-06 3 0.64427E-08 0.16239E-06 0.66492E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.5096e-10 1.5096e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.9933e-21 5.9933e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.403000000E+02 TIME STEP NUMBER 403 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 24 0.30511E-06 0.13748E-15 0.51130E-07 c Velocity[X] 0.75295E-16 c Velocity[Y] 0.62188E-16 c Velocity[Z] 0.13307E-37 c Pressure 0.19246E-06 3 0.62437E-08 0.15746E-06 0.64319E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.4255e-10 1.4255e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.8598e-21 5.8598e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.404000000E+02 TIME STEP NUMBER 404 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 24 0.29601E-06 0.12397E-15 0.48553E-07 c Velocity[X] 0.60178E-16 c Velocity[Y] 0.63794E-16 c Velocity[Z] 0.19829E-37 c Pressure 0.18672E-06 3 0.60632E-08 0.15277E-06 0.62486E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.3814e-10 1.3814e-10 v Velocity[Z] -1.4597e-17 1.225e-17 2.9092e-21 2.9092e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.405000000E+02 TIME STEP NUMBER 405 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 24 0.28719E-06 0.11653E-15 0.47073E-07 c Velocity[X] 0.56278E-16 c Velocity[Y] 0.60255E-16 c Velocity[Z] 0.15666E-37 c Pressure 0.18116E-06 3 0.58882E-08 0.14821E-06 0.60716E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.3442e-10 1.3442e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.3651e-21 5.3651e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.406000000E+02 TIME STEP NUMBER 406 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 23 0.27835E-06 0.11505E-15 0.46772E-07 c Velocity[X] 0.63449E-16 c Velocity[Y] 0.51597E-16 c Velocity[Z] 0.96789E-38 c Pressure 0.17564E-06 3 0.57048E-08 0.14370E-06 0.58714E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.2686e-10 1.2686e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.1355e-21 5.1355e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.407000000E+02 TIME STEP NUMBER 407 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 23 0.27006E-06 0.10318E-15 0.44294E-07 c Velocity[X] 0.49893E-16 c Velocity[Y] 0.53284E-16 c Velocity[Z] 0.15016E-37 c Pressure 0.17041E-06 3 0.55399E-08 0.13942E-06 0.57046E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.2317e-10 1.2317e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3387e-21 4.3387e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.408000000E+02 TIME STEP NUMBER 408 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 23 0.26203E-06 0.96969E-16 0.42940E-07 c Velocity[X] 0.46608E-16 c Velocity[Y] 0.50360E-16 c Velocity[Z] 0.23311E-37 c Pressure 0.16533E-06 3 0.53801E-08 0.13526E-06 0.55438E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.2013e-10 1.2013e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.3515e-21 5.3515e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.409000000E+02 TIME STEP NUMBER 409 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 22 0.25391E-06 0.96336E-16 0.42800E-07 c Velocity[X] 0.53546E-16 c Velocity[Y] 0.42790E-16 c Velocity[Z] 0.11758E-37 c Pressure 0.16027E-06 3 0.52110E-08 0.13112E-06 0.53591E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.1331e-10 1.1331e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.8818e-21 3.8818e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.410000000E+02 TIME STEP NUMBER 410 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 22 0.24636E-06 0.85849E-16 0.40403E-07 c Velocity[X] 0.41347E-16 c Velocity[Y] 0.44502E-16 c Velocity[Z] 0.27462E-37 c Pressure 0.15550E-06 3 0.50606E-08 0.12722E-06 0.52075E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062203 0.062203 1.1023e-10 1.1023e-10 v Velocity[Z] -1.4597e-17 1.225e-17 7.1003e-21 7.1003e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.411000000E+02 TIME STEP NUMBER 411 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 22 0.23904E-06 0.80666E-16 0.39165E-07 c Velocity[X] 0.38574E-16 c Velocity[Y] 0.42092E-16 c Velocity[Z] 0.14343E-37 c Pressure 0.15087E-06 3 0.49148E-08 0.12343E-06 0.50615E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 1.0776e-10 1.0776e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.7515e-21 3.7515e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.412000000E+02 TIME STEP NUMBER 412 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 21 0.23159E-06 0.80734E-16 0.39181E-07 c Velocity[X] 0.45264E-16 c Velocity[Y] 0.35469E-16 c Velocity[Z] 0.14841E-37 c Pressure 0.14622E-06 3 0.47588E-08 0.11963E-06 0.48908E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 1.0158e-10 1.0158e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9872e-21 4.9872e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.413000000E+02 TIME STEP NUMBER 413 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 21 0.22471E-06 0.71408E-16 0.36849E-07 c Velocity[X] 0.34247E-16 c Velocity[Y] 0.37161E-16 c Velocity[Z] 0.89957E-38 c Pressure 0.14187E-06 3 0.46216E-08 0.11607E-06 0.47531E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 9.9005e-11 9.9005e-11 v Velocity[Z] -1.4597e-17 1.225e-17 4.456e-21 4.456e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.414000000E+02 TIME STEP NUMBER 414 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 21 0.21805E-06 0.67081E-16 0.35715E-07 c Velocity[X] 0.31899E-16 c Velocity[Y] 0.35181E-16 c Velocity[Z] 0.16799E-37 c Pressure 0.13766E-06 3 0.44888E-08 0.11262E-06 0.46207E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 9.7028e-11 9.7028e-11 v Velocity[Z] -1.4597e-17 1.225e-17 7.7372e-21 7.7372e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.415000000E+02 TIME STEP NUMBER 415 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 21 0.21159E-06 0.63148E-16 0.34652E-07 c Velocity[X] 0.30055E-16 c Velocity[Y] 0.33093E-16 c Velocity[Z] 0.19812E-37 c Pressure 0.13356E-06 3 0.43597E-08 0.10927E-06 0.44920E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 9.5192e-11 9.5192e-11 v Velocity[Z] -1.4597e-17 1.225e-17 4.9937e-21 4.9937e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.416000000E+02 TIME STEP NUMBER 416 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 20 0.20495E-06 0.63792E-16 0.34828E-07 c Velocity[X] 0.36174E-16 c Velocity[Y] 0.27618E-16 c Velocity[Z] 0.23159E-37 c Pressure 0.12942E-06 3 0.42197E-08 0.10588E-06 0.43383E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 8.9703e-11 8.9703e-11 v Velocity[Z] -1.4597e-17 1.225e-17 3.7681e-21 3.7681e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.417000000E+02 TIME STEP NUMBER 417 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 20 0.19887E-06 0.55903E-16 0.32604E-07 c Velocity[X] 0.26730E-16 c Velocity[Y] 0.29173E-16 c Velocity[Z] 0.22198E-37 c Pressure 0.12558E-06 3 0.40983E-08 0.10274E-06 0.42167E-08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 8.7623e-11 8.7623e-11 v Velocity[Z] -1.4597e-17 1.225e-17 6.255e-21 6.255e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.418000000E+02 TIME STEP NUMBER 418 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 20 0.19299E-06 0.12493E-12 0.15413E-05 c Velocity[X] 0.62780E-13 c Velocity[Y] 0.62152E-13 c Velocity[Z] 0.19018E-37 c Pressure 0.12185E-06 0 0.99688E-07 0.99688E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 1.5448e-10 1.5448e-10 v Velocity[Z] -1.4597e-17 1.225e-17 2.6715e-21 2.6715e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.419000000E+02 TIME STEP NUMBER 419 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 7 0.34866E-07 0.16303E-14 0.17607E-06 c Velocity[X] 0.74404E-15 c Velocity[Y] 0.88631E-15 c Velocity[Z] 0.29598E-37 c Pressure 0.11624E-06 0 0.95102E-07 0.95102E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 1.8461e-10 1.8461e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.8751e-21 4.8751e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.420000000E+02 TIME STEP NUMBER 420 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.77120E-08 0.11713E-16 0.14924E-07 c Velocity[X] 0.34013E-17 c Velocity[Y] 0.83116E-17 c Velocity[Z] 0.12338E-37 c Pressure 0.11663E-06 0 0.95421E-07 0.95421E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 1.8874e-10 1.8874e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.0301e-21 5.0301e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.421000000E+02 TIME STEP NUMBER 421 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.59578E-08 0.34736E-17 0.81272E-08 c Velocity[X] 0.27015E-17 c Velocity[Y] 0.77211E-18 c Velocity[Z] 0.10225E-37 c Pressure 0.11687E-06 0 0.95611E-07 0.95611E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 1.9282e-10 1.9282e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5924e-21 5.5924e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.422000000E+02 TIME STEP NUMBER 422 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.52924E-08 0.27551E-17 0.72380E-08 c Velocity[X] 0.23568E-17 c Velocity[Y] 0.39828E-18 c Velocity[Z] 0.13625E-37 c Pressure 0.11702E-06 0 0.95741E-07 0.95741E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 1.9675e-10 1.9675e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.0215e-21 6.0215e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.423000000E+02 TIME STEP NUMBER 423 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.48448E-08 0.23193E-17 0.66410E-08 c Velocity[X] 0.20744E-17 c Velocity[Y] 0.24492E-18 c Velocity[Z] 0.27256E-37 c Pressure 0.11714E-06 0 0.95835E-07 0.95835E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.0046e-10 2.0046e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.0726e-21 5.0726e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.424000000E+02 TIME STEP NUMBER 424 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.44869E-08 0.19933E-17 0.61565E-08 c Velocity[X] 0.18313E-17 c Velocity[Y] 0.16201E-18 c Velocity[Z] 0.14375E-37 c Pressure 0.11723E-06 0 0.95906E-07 0.95906E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.0395e-10 2.0395e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.4422e-21 6.4422e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.425000000E+02 TIME STEP NUMBER 425 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.41802E-08 0.17316E-17 0.57382E-08 c Velocity[X] 0.16193E-17 c Velocity[Y] 0.11229E-18 c Velocity[Z] 0.10216E-37 c Pressure 0.11729E-06 0 0.95960E-07 0.95960E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.0725e-10 2.0725e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.5486e-21 4.5486e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.426000000E+02 TIME STEP NUMBER 426 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.39082E-08 0.15142E-17 0.53659E-08 c Velocity[X] 0.14337E-17 c Velocity[Y] 0.80452E-19 c Velocity[Z] 0.17843E-37 c Pressure 0.11734E-06 0 0.96003E-07 0.96003E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.1037e-10 2.1037e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.624e-21 3.624e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.427000000E+02 TIME STEP NUMBER 427 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.36627E-08 0.13300E-17 0.50289E-08 c Velocity[X] 0.12709E-17 c Velocity[Y] 0.59087E-19 c Velocity[Z] 0.92731E-38 c Pressure 0.11738E-06 0 0.96036E-07 0.96036E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.1334e-10 2.1334e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.3965e-21 5.3965e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.428000000E+02 TIME STEP NUMBER 428 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.34387E-08 0.11722E-17 0.47211E-08 c Velocity[X] 0.11279E-17 c Velocity[Y] 0.44247E-19 c Velocity[Z] 0.12935E-37 c Pressure 0.11742E-06 0 0.96063E-07 0.96063E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.1615e-10 2.1615e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.8353e-21 5.8353e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.429000000E+02 TIME STEP NUMBER 429 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.32330E-08 0.10359E-17 0.44381E-08 c Velocity[X] 0.10022E-17 c Velocity[Y] 0.33664E-19 c Velocity[Z] 0.92818E-38 c Pressure 0.11744E-06 0 0.96085E-07 0.96085E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.1883e-10 2.1883e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7778e-21 5.7778e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.430000000E+02 TIME STEP NUMBER 430 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.30433E-08 0.91752E-18 0.41769E-08 c Velocity[X] 0.89157E-18 c Velocity[Y] 0.25957E-19 c Velocity[Z] 0.21724E-37 c Pressure 0.11747E-06 0 0.96103E-07 0.96103E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.2138e-10 2.2138e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.4285e-21 5.4285e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.431000000E+02 TIME STEP NUMBER 431 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.28677E-08 0.81438E-18 0.39352E-08 c Velocity[X] 0.79413E-18 c Velocity[Y] 0.20248E-19 c Velocity[Z] 0.81185E-38 c Pressure 0.11748E-06 0 0.96118E-07 0.96118E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.2382e-10 2.2382e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.4661e-21 5.4661e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.432000000E+02 TIME STEP NUMBER 432 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.27049E-08 0.72417E-18 0.37108E-08 c Velocity[X] 0.70821E-18 c Velocity[Y] 0.15959E-19 c Velocity[Z] 0.10263E-37 c Pressure 0.11750E-06 0 0.96130E-07 0.96130E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.2615e-10 2.2615e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3596e-21 4.3596e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.433000000E+02 TIME STEP NUMBER 433 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.25535E-08 0.64508E-18 0.35023E-08 c Velocity[X] 0.63238E-18 c Velocity[Y] 0.12696E-19 c Velocity[Z] 0.97689E-38 c Pressure 0.11751E-06 0 0.96139E-07 0.96139E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.2837e-10 2.2837e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.7634e-21 4.7634e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.434000000E+02 TIME STEP NUMBER 434 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.24126E-08 0.57556E-18 0.33082E-08 c Velocity[X] 0.56537E-18 c Velocity[Y] 0.10186E-19 c Velocity[Z] 0.79286E-38 c Pressure 0.11752E-06 0 0.96148E-07 0.96148E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.305e-10 2.305e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9107e-21 4.9107e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.435000000E+02 TIME STEP NUMBER 435 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.22813E-08 0.51433E-18 0.31273E-08 c Velocity[X] 0.50609E-18 c Velocity[Y] 0.82366E-20 c Velocity[Z] 0.12059E-37 c Pressure 0.11753E-06 0 0.96154E-07 0.96154E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.3253e-10 2.3253e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7163e-21 5.7163e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.436000000E+02 TIME STEP NUMBER 436 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.21588E-08 0.46029E-18 0.29585E-08 c Velocity[X] 0.45358E-18 c Velocity[Y] 0.67091E-20 c Velocity[Z] 0.13551E-37 c Pressure 0.11754E-06 0 0.96160E-07 0.96160E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.3448e-10 2.3448e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.2793e-21 5.2793e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.437000000E+02 TIME STEP NUMBER 437 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.20444E-08 0.41253E-18 0.28008E-08 c Velocity[X] 0.40702E-18 c Velocity[Y] 0.55023E-20 c Velocity[Z] 0.76764E-38 c Pressure 0.11754E-06 0 0.96165E-07 0.96165E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.3634e-10 2.3634e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.6742e-21 4.6742e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.438000000E+02 TIME STEP NUMBER 438 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.19373E-08 0.37023E-18 0.26533E-08 c Velocity[X] 0.36569E-18 c Velocity[Y] 0.45416E-20 c Velocity[Z] 0.19438E-37 c Pressure 0.11755E-06 0 0.96169E-07 0.96169E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.3813e-10 2.3813e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.5272e-21 4.5272e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.439000000E+02 TIME STEP NUMBER 439 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.18372E-08 0.33272E-18 0.25153E-08 c Velocity[X] 0.32894E-18 c Velocity[Y] 0.37714E-20 c Velocity[Z] 0.16180E-37 c Pressure 0.11755E-06 0 0.96172E-07 0.96172E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.3985e-10 2.3985e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.1975e-21 5.1975e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.440000000E+02 TIME STEP NUMBER 440 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.17433E-08 0.29940E-18 0.23860E-08 c Velocity[X] 0.29625E-18 c Velocity[Y] 0.31499E-20 c Velocity[Z] 0.19884E-37 c Pressure 0.11755E-06 0 0.96174E-07 0.96174E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.4149e-10 2.4149e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.1817e-21 5.1817e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.441000000E+02 TIME STEP NUMBER 441 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.16554E-08 0.26976E-18 0.22648E-08 c Velocity[X] 0.26711E-18 c Velocity[Y] 0.26451E-20 c Velocity[Z] 0.15255E-37 c Pressure 0.11756E-06 0 0.96177E-07 0.96177E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.4307e-10 2.4307e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.9414e-21 5.9414e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.442000000E+02 TIME STEP NUMBER 442 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.15729E-08 0.24336E-18 0.21511E-08 c Velocity[X] 0.24112E-18 c Velocity[Y] 0.22327E-20 c Velocity[Z] 0.12429E-37 c Pressure 0.11756E-06 0 0.96178E-07 0.96178E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.4458e-10 2.4458e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.3258e-21 5.3258e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.443000000E+02 TIME STEP NUMBER 443 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.14954E-08 0.21980E-18 0.20444E-08 c Velocity[X] 0.21791E-18 c Velocity[Y] 0.18939E-20 c Velocity[Z] 0.82703E-38 c Pressure 0.11756E-06 0 0.96180E-07 0.96180E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.4604e-10 2.4604e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.0632e-21 5.0632e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.444000000E+02 TIME STEP NUMBER 444 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.14226E-08 0.19877E-18 0.19441E-08 c Velocity[X] 0.19715E-18 c Velocity[Y] 0.16140E-20 c Velocity[Z] 0.52958E-38 c Pressure 0.11756E-06 0 0.96181E-07 0.96181E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.4743e-10 2.4743e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.5265e-21 4.5265e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.445000000E+02 TIME STEP NUMBER 445 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.13541E-08 0.17995E-18 0.18498E-08 c Velocity[X] 0.17857E-18 c Velocity[Y] 0.13815E-20 c Velocity[Z] 0.12151E-37 c Pressure 0.11756E-06 0 0.96182E-07 0.96182E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.4878e-10 2.4878e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.2352e-21 4.2352e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.446000000E+02 TIME STEP NUMBER 446 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.12897E-08 0.16310E-18 0.17611E-08 c Velocity[X] 0.16192E-18 c Velocity[Y] 0.11875E-20 c Velocity[Z] 0.15647E-37 c Pressure 0.11756E-06 0 0.96182E-07 0.96182E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.5006e-10 2.5006e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.6006e-21 5.6006e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.447000000E+02 TIME STEP NUMBER 447 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.12290E-08 0.14800E-18 0.16775E-08 c Velocity[X] 0.14697E-18 c Velocity[Y] 0.10249E-20 c Velocity[Z] 0.11257E-37 c Pressure 0.11756E-06 0 0.96183E-07 0.96183E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.513e-10 2.513e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.5072e-21 4.5072e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.448000000E+02 TIME STEP NUMBER 448 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.11719E-08 0.13443E-18 0.15988E-08 c Velocity[X] 0.13354E-18 c Velocity[Y] 0.88782E-21 c Velocity[Z] 0.11915E-37 c Pressure 0.11756E-06 0 0.96183E-07 0.96183E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.525e-10 2.525e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.2435e-21 5.2435e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.449000000E+02 TIME STEP NUMBER 449 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.11180E-08 0.12224E-18 0.15246E-08 c Velocity[X] 0.12147E-18 c Velocity[Y] 0.77185E-21 c Velocity[Z] 0.65164E-38 c Pressure 0.11756E-06 0 0.96183E-07 0.96183E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.5364e-10 2.5364e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.105e-21 6.105e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.450000000E+02 TIME STEP NUMBER 450 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.10672E-08 0.11127E-18 0.14546E-08 c Velocity[X] 0.11060E-18 c Velocity[Y] 0.67332E-21 c Velocity[Z] 0.15830E-37 c Pressure 0.11756E-06 0 0.96183E-07 0.96183E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.5474e-10 2.5474e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.8325e-21 6.8325e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.451000000E+02 TIME STEP NUMBER 451 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.10192E-08 0.10138E-18 0.13885E-08 c Velocity[X] 0.10080E-18 c Velocity[Y] 0.58924E-21 c Velocity[Z] 0.13190E-37 c Pressure 0.11756E-06 0 0.96183E-07 0.96183E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.558e-10 2.558e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.1278e-21 6.1278e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.452000000E+02 TIME STEP NUMBER 452 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.97383E-09 0.92469E-19 0.13260E-08 c Velocity[X] 0.91952E-19 c Velocity[Y] 0.51724E-21 c Velocity[Z] 0.15432E-37 c Pressure 0.11756E-06 0 0.96183E-07 0.96183E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.5682e-10 2.5682e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.3088e-21 4.3088e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.453000000E+02 TIME STEP NUMBER 453 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.93098E-09 0.84418E-19 0.12670E-08 c Velocity[X] 0.83963E-19 c Velocity[Y] 0.45533E-21 c Velocity[Z] 0.16162E-37 c Pressure 0.11756E-06 0 0.96182E-07 0.96182E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.5781e-10 2.5781e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.8952e-21 3.8952e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.454000000E+02 TIME STEP NUMBER 454 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.89045E-09 0.77140E-19 0.12111E-08 c Velocity[X] 0.76738E-19 c Velocity[Y] 0.40193E-21 c Velocity[Z] 0.13025E-37 c Pressure 0.11756E-06 0 0.96182E-07 0.96182E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.5875e-10 2.5875e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9954e-21 4.9954e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.455000000E+02 TIME STEP NUMBER 455 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.85211E-09 0.70554E-19 0.11583E-08 c Velocity[X] 0.70199E-19 c Velocity[Y] 0.35570E-21 c Velocity[Z] 0.13000E-37 c Pressure 0.11756E-06 0 0.96182E-07 0.96182E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.5966e-10 2.5966e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.451e-21 5.451e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.456000000E+02 TIME STEP NUMBER 456 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.81580E-09 0.64588E-19 0.11082E-08 c Velocity[X] 0.64273E-19 c Velocity[Y] 0.31555E-21 c Velocity[Z] 0.69184E-38 c Pressure 0.11756E-06 0 0.96181E-07 0.96181E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6054e-10 2.6054e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.8504e-21 4.8504e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.457000000E+02 TIME STEP NUMBER 457 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.78140E-09 0.59178E-19 0.10608E-08 c Velocity[X] 0.58897E-19 c Velocity[Y] 0.28058E-21 c Velocity[Z] 0.72585E-38 c Pressure 0.11756E-06 0 0.96181E-07 0.96181E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6139e-10 2.6139e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9433e-21 4.9433e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.458000000E+02 TIME STEP NUMBER 458 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.74880E-09 0.54267E-19 0.10158E-08 c Velocity[X] 0.54017E-19 c Velocity[Y] 0.25002E-21 c Velocity[Z] 0.19351E-37 c Pressure 0.11756E-06 0 0.96180E-07 0.96180E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.622e-10 2.622e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5189e-21 5.5189e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.459000000E+02 TIME STEP NUMBER 459 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.71788E-09 0.49804E-19 0.97315E-09 c Velocity[X] 0.49581E-19 c Velocity[Y] 0.22325E-21 c Velocity[Z] 0.95304E-38 c Pressure 0.11756E-06 0 0.96180E-07 0.96180E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6299e-10 2.6299e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.6299e-21 5.6299e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.460000000E+02 TIME STEP NUMBER 460 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.68854E-09 0.45745E-19 0.93266E-09 c Velocity[X] 0.45546E-19 c Velocity[Y] 0.19973E-21 c Velocity[Z] 0.21212E-37 c Pressure 0.11756E-06 0 0.96179E-07 0.96179E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6374e-10 2.6374e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.8363e-21 4.8363e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.461000000E+02 TIME STEP NUMBER 461 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.66069E-09 0.42050E-19 0.89420E-09 c Velocity[X] 0.41871E-19 c Velocity[Y] 0.17902E-21 c Velocity[Z] 0.99229E-38 c Pressure 0.11756E-06 0 0.96179E-07 0.96179E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6447e-10 2.6447e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.7414e-21 4.7414e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.462000000E+02 TIME STEP NUMBER 462 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.63423E-09 0.38683E-19 0.85765E-09 c Velocity[X] 0.38522E-19 c Velocity[Y] 0.16074E-21 c Velocity[Z] 0.10863E-37 c Pressure 0.11756E-06 0 0.96178E-07 0.96178E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6518e-10 2.6518e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.1379e-21 4.1379e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.463000000E+02 TIME STEP NUMBER 463 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.60910E-09 0.35612E-19 0.82290E-09 c Velocity[X] 0.35468E-19 c Velocity[Y] 0.14457E-21 c Velocity[Z] 0.14170E-37 c Pressure 0.11756E-06 0 0.96178E-07 0.96178E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6586e-10 2.6586e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.1441e-21 5.1441e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.464000000E+02 TIME STEP NUMBER 464 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.58520E-09 0.32809E-19 0.78985E-09 c Velocity[X] 0.32679E-19 c Velocity[Y] 0.13022E-21 c Velocity[Z] 0.14277E-37 c Pressure 0.11756E-06 0 0.96177E-07 0.96177E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6651e-10 2.6651e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.675e-21 5.675e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.465000000E+02 TIME STEP NUMBER 465 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.56247E-09 0.30248E-19 0.75839E-09 c Velocity[X] 0.30130E-19 c Velocity[Y] 0.11748E-21 c Velocity[Z] 0.11761E-37 c Pressure 0.11756E-06 0 0.96176E-07 0.96176E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6714e-10 2.6714e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.6708e-21 4.6708e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.466000000E+02 TIME STEP NUMBER 466 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.54085E-09 0.27905E-19 0.72844E-09 c Velocity[X] 0.27799E-19 c Velocity[Y] 0.10614E-21 c Velocity[Z] 0.71310E-38 c Pressure 0.11756E-06 0 0.96176E-07 0.96176E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6775e-10 2.6775e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.7605e-21 4.7605e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.467000000E+02 TIME STEP NUMBER 467 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.52026E-09 0.25762E-19 0.69990E-09 c Velocity[X] 0.25666E-19 c Velocity[Y] 0.96017E-22 c Velocity[Z] 0.11532E-37 c Pressure 0.11755E-06 0 0.96175E-07 0.96175E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6834e-10 2.6834e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9202e-21 4.9202e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.468000000E+02 TIME STEP NUMBER 468 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.50066E-09 0.23799E-19 0.67271E-09 c Velocity[X] 0.23712E-19 c Velocity[Y] 0.86976E-22 c Velocity[Z] 0.22525E-37 c Pressure 0.11755E-06 0 0.96175E-07 0.96175E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6891e-10 2.6891e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.1376e-21 4.1376e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.469000000E+02 TIME STEP NUMBER 469 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.48198E-09 0.21999E-19 0.64677E-09 c Velocity[X] 0.21920E-19 c Velocity[Y] 0.78884E-22 c Velocity[Z] 0.15839E-37 c Pressure 0.11755E-06 0 0.96174E-07 0.96174E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6946e-10 2.6946e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.8957e-21 5.8957e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.470000000E+02 TIME STEP NUMBER 470 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.46418E-09 0.20348E-19 0.62203E-09 c Velocity[X] 0.20276E-19 c Velocity[Y] 0.71630E-22 c Velocity[Z] 0.11363E-37 c Pressure 0.11755E-06 0 0.96174E-07 0.96174E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.6999e-10 2.6999e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9546e-21 4.9546e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.471000000E+02 TIME STEP NUMBER 471 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.44722E-09 0.18832E-19 0.59841E-09 c Velocity[X] 0.18767E-19 c Velocity[Y] 0.65116E-22 c Velocity[Z] 0.84775E-38 c Pressure 0.11755E-06 0 0.96173E-07 0.96173E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.705e-10 2.705e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.7854e-21 4.7854e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.472000000E+02 TIME STEP NUMBER 472 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.43103E-09 0.17440E-19 0.57586E-09 c Velocity[X] 0.17380E-19 c Velocity[Y] 0.59259E-22 c Velocity[Z] 0.70808E-38 c Pressure 0.11755E-06 0 0.96173E-07 0.96173E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7099e-10 2.7099e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.1009e-21 5.1009e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.473000000E+02 TIME STEP NUMBER 473 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.41559E-09 0.16159E-19 0.55432E-09 c Velocity[X] 0.16105E-19 c Velocity[Y] 0.53985E-22 c Velocity[Z] 0.10880E-37 c Pressure 0.11755E-06 0 0.96172E-07 0.96172E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7147e-10 2.7147e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.0239e-21 6.0239e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.474000000E+02 TIME STEP NUMBER 474 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.40086E-09 0.14981E-19 0.53373E-09 c Velocity[X] 0.14932E-19 c Velocity[Y] 0.49230E-22 c Velocity[Z] 0.10668E-37 c Pressure 0.11755E-06 0 0.96171E-07 0.96171E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7193e-10 2.7193e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.4307e-21 5.4307e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.475000000E+02 TIME STEP NUMBER 475 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.38680E-09 0.13897E-19 0.51405E-09 c Velocity[X] 0.13852E-19 c Velocity[Y] 0.44936E-22 c Velocity[Z] 0.19789E-37 c Pressure 0.11755E-06 0 0.96171E-07 0.96171E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7238e-10 2.7238e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.6606e-21 4.6606e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.476000000E+02 TIME STEP NUMBER 476 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.37336E-09 0.12898E-19 0.49523E-09 c Velocity[X] 0.12857E-19 c Velocity[Y] 0.41055E-22 c Velocity[Z] 0.16970E-37 c Pressure 0.11755E-06 0 0.96170E-07 0.96170E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7281e-10 2.7281e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9613e-21 4.9613e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.477000000E+02 TIME STEP NUMBER 477 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.36054E-09 0.11976E-19 0.47721E-09 c Velocity[X] 0.11939E-19 c Velocity[Y] 0.37542E-22 c Velocity[Z] 0.11705E-37 c Pressure 0.11755E-06 0 0.96170E-07 0.96170E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7322e-10 2.7322e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.4849e-21 5.4849e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.478000000E+02 TIME STEP NUMBER 478 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.34828E-09 0.11127E-19 0.45997E-09 c Velocity[X] 0.11092E-19 c Velocity[Y] 0.34359E-22 c Velocity[Z] 0.19467E-37 c Pressure 0.11755E-06 0 0.96169E-07 0.96169E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7362e-10 2.7362e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.5656e-21 6.5656e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.479000000E+02 TIME STEP NUMBER 479 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.33658E-09 0.10342E-19 0.44347E-09 c Velocity[X] 0.10311E-19 c Velocity[Y] 0.31472E-22 c Velocity[Z] 0.12188E-37 c Pressure 0.11755E-06 0 0.96169E-07 0.96169E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7401e-10 2.7401e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5568e-21 5.5568e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.480000000E+02 TIME STEP NUMBER 480 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.32538E-09 0.96180E-20 0.42765E-09 c Velocity[X] 0.95892E-20 c Velocity[Y] 0.28850E-22 c Velocity[Z] 0.11517E-37 c Pressure 0.11755E-06 0 0.96169E-07 0.96169E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7439e-10 2.7439e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.3226e-21 6.3226e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.481000000E+02 TIME STEP NUMBER 481 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.31468E-09 0.89486E-20 0.41250E-09 c Velocity[X] 0.89221E-20 c Velocity[Y] 0.26468E-22 c Velocity[Z] 0.10904E-37 c Pressure 0.11755E-06 0 0.96168E-07 0.96168E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7475e-10 2.7475e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.3359e-21 6.3359e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.482000000E+02 TIME STEP NUMBER 482 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.30445E-09 0.83296E-20 0.39798E-09 c Velocity[X] 0.83053E-20 c Velocity[Y] 0.24299E-22 c Velocity[Z] 0.90098E-38 c Pressure 0.11755E-06 0 0.96168E-07 0.96168E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.751e-10 2.751e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.694e-21 6.694e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.483000000E+02 TIME STEP NUMBER 483 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.29467E-09 0.77568E-20 0.38405E-09 c Velocity[X] 0.77345E-20 c Velocity[Y] 0.22325E-22 c Velocity[Z] 0.11630E-37 c Pressure 0.11754E-06 0 0.96167E-07 0.96167E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7544e-10 2.7544e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.576e-21 6.576e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.484000000E+02 TIME STEP NUMBER 484 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.28531E-09 0.72267E-20 0.37070E-09 c Velocity[X] 0.72062E-20 c Velocity[Y] 0.20524E-22 c Velocity[Z] 0.18086E-37 c Pressure 0.11754E-06 0 0.96167E-07 0.96167E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7577e-10 2.7577e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.7246e-21 5.7246e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.485000000E+02 TIME STEP NUMBER 485 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.27636E-09 0.67357E-20 0.35788E-09 c Velocity[X] 0.67168E-20 c Velocity[Y] 0.18882E-22 c Velocity[Z] 0.12922E-37 c Pressure 0.11754E-06 0 0.96166E-07 0.96166E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7608e-10 2.7608e-10 v Velocity[Z] -1.4597e-17 1.225e-17 3.9404e-21 3.9404e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.486000000E+02 TIME STEP NUMBER 486 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.26780E-09 0.62807E-20 0.34558E-09 c Velocity[X] 0.62633E-20 c Velocity[Y] 0.17382E-22 c Velocity[Z] 0.11877E-37 c Pressure 0.11754E-06 0 0.96166E-07 0.96166E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7639e-10 2.7639e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5289e-21 5.5289e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.487000000E+02 TIME STEP NUMBER 487 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.25961E-09 0.58588E-20 0.33378E-09 c Velocity[X] 0.58428E-20 c Velocity[Y] 0.16012E-22 c Velocity[Z] 0.17662E-37 c Pressure 0.11754E-06 0 0.96166E-07 0.96166E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7669e-10 2.7669e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.0823e-21 4.0823e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.488000000E+02 TIME STEP NUMBER 488 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.25177E-09 0.54676E-20 0.32244E-09 c Velocity[X] 0.54528E-20 c Velocity[Y] 0.14758E-22 c Velocity[Z] 0.13074E-37 c Pressure 0.11754E-06 0 0.96165E-07 0.96165E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7697e-10 2.7697e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9081e-21 4.9081e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.489000000E+02 TIME STEP NUMBER 489 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.24427E-09 0.51044E-20 0.31155E-09 c Velocity[X] 0.50908E-20 c Velocity[Y] 0.13611E-22 c Velocity[Z] 0.15816E-37 c Pressure 0.11754E-06 0 0.96165E-07 0.96165E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7725e-10 2.7725e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.3563e-21 5.3563e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.490000000E+02 TIME STEP NUMBER 490 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.23709E-09 0.47673E-20 0.30108E-09 c Velocity[X] 0.47547E-20 c Velocity[Y] 0.12560E-22 c Velocity[Z] 0.18756E-37 c Pressure 0.11754E-06 0 0.96165E-07 0.96165E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7752e-10 2.7752e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.1268e-21 5.1268e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.491000000E+02 TIME STEP NUMBER 491 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.23022E-09 0.44541E-20 0.29102E-09 c Velocity[X] 0.44425E-20 c Velocity[Y] 0.11597E-22 c Velocity[Z] 0.14044E-37 c Pressure 0.11754E-06 0 0.96164E-07 0.96164E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7778e-10 2.7778e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.6672e-21 5.6672e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.492000000E+02 TIME STEP NUMBER 492 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.22365E-09 0.41631E-20 0.28136E-09 c Velocity[X] 0.41524E-20 c Velocity[Y] 0.10712E-22 c Velocity[Z] 0.14301E-37 c Pressure 0.11754E-06 0 0.96164E-07 0.96164E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7803e-10 2.7803e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9652e-21 4.9652e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.493000000E+02 TIME STEP NUMBER 493 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.21736E-09 0.38925E-20 0.27206E-09 c Velocity[X] 0.38826E-20 c Velocity[Y] 0.99015E-23 c Velocity[Z] 0.12997E-37 c Pressure 0.11754E-06 0 0.96164E-07 0.96164E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7827e-10 2.7827e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.3951e-21 5.3951e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.494000000E+02 TIME STEP NUMBER 494 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.21134E-09 0.36409E-20 0.26312E-09 c Velocity[X] 0.36317E-20 c Velocity[Y] 0.91561E-23 c Velocity[Z] 0.10076E-37 c Pressure 0.11754E-06 0 0.96163E-07 0.96163E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7851e-10 2.7851e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.5809e-21 5.5809e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.495000000E+02 TIME STEP NUMBER 495 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.20558E-09 0.34067E-20 0.25452E-09 c Velocity[X] 0.33982E-20 c Velocity[Y] 0.84715E-23 c Velocity[Z] 0.13358E-37 c Pressure 0.11754E-06 0 0.96163E-07 0.96163E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7874e-10 2.7874e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.1135e-21 6.1135e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.496000000E+02 TIME STEP NUMBER 496 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.20006E-09 0.31888E-20 0.24624E-09 c Velocity[X] 0.31809E-20 c Velocity[Y] 0.78414E-23 c Velocity[Z] 0.99229E-38 c Pressure 0.11754E-06 0 0.96163E-07 0.96163E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7896e-10 2.7896e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9059e-21 4.9059e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.497000000E+02 TIME STEP NUMBER 497 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.19479E-09 0.29858E-20 0.23827E-09 c Velocity[X] 0.29785E-20 c Velocity[Y] 0.72620E-23 c Velocity[Z] 0.11230E-37 c Pressure 0.11754E-06 0 0.96162E-07 0.96162E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7917e-10 2.7917e-10 v Velocity[Z] -1.4597e-17 1.225e-17 4.9644e-21 4.9644e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.498000000E+02 TIME STEP NUMBER 498 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.18974E-09 0.27968E-20 0.23061E-09 c Velocity[X] 0.27900E-20 c Velocity[Y] 0.67281E-23 c Velocity[Z] 0.77420E-38 c Pressure 0.11754E-06 0 0.96162E-07 0.96162E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7938e-10 2.7938e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.8841e-21 5.8841e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.499000000E+02 TIME STEP NUMBER 499 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.18492E-09 0.26205E-20 0.22323E-09 c Velocity[X] 0.26143E-20 c Velocity[Y] 0.62367E-23 c Velocity[Z] 0.14159E-37 c Pressure 0.11754E-06 0 0.96162E-07 0.96162E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7958e-10 2.7958e-10 v Velocity[Z] -1.4597e-17 1.225e-17 6.8175e-21 6.8175e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 INSTANT 0.500000000E+02 TIME STEP NUMBER 500 ============================================================= Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Inlet" in the selection criteria: "Inlet" does not correspond to any boundary face. Code_Saturne: /home/tsubasa/Code_Saturne/code_saturne-6.0.5/src/base/cs_selector.c:111: Warning The group "Outlet" in the selection criteria: "Outlet" does not correspond to any boundary face. ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 20 -0.666667000E+00 Smooth wall 5 400 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 8000 0.000000000E+00 Free outlet 3 20 0.666666993E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19944E+01 0.37311E+01 Friction velocity uk : 0.19944E+01 0.37311E+01 Dimensionless distance yplus : 0.49859E-01 0.93277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 400 Total number of wall faces : 400 ------------------------------------------------------------ Write final restart files checkpoint at iteration 500, Physical time 0.50000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 500: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62388E+01 1 0.18030E-09 0.24563E-20 0.21612E-09 c Velocity[X] 0.24506E-20 c Velocity[Y] 0.57833E-23 c Velocity[Z] 0.84254E-38 c Pressure 0.11754E-06 0 0.96162E-07 0.96162E-07 0.00000E+00 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ----------- -------------- -------------- -------------- -------------- v Velocity[X] 0.099436 1.0009 0.66381 0.66381 v Velocity[Y] -0.062202 0.062202 2.7977e-10 2.7977e-10 v Velocity[Z] -1.4597e-17 1.225e-17 5.409e-21 5.409e-21 v ǁVelocityǁ 0.099436 1.0009 0.66386 0.66386 v Pressure 199.01 80367 39824 39824 v CourantNb 1.8175 19.978 13.418 13.418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 801.99 2017.3 1573.4 1573.4 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation