command: ./cs_solver --mpi *************************************************************** (R) Code_Saturne Version 6.0.4 Copyright (C) 1998-2019 EDF S.A., France revision 6.0.4-4743b4795 build vie 02 oct 2020 22:39:59 -03 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 20 oct 2020 19:54:41 -03 System: Linux 4.13.0-38-generic (Ubuntu 17.10) Machine: valkyrie Processor: model name : Intel(R) Core(TM) i7-8550U CPU @ 1.80GHz Memory: 15781 MB User: lgarelli (lgarelli) Directory: /home/lgarelli/RUNS_local/Code_Saturne/Internal_coup_Gustavo/Interncal_coupling_example/RESU/20201020-1954 MPI ranks: 2 (appnum attribute: 0) OpenMP threads: 1 Processors/node: 4 I/O read method: collective MPI-IO (explicit offsets) I/O write method: collective MPI-IO (explicit offsets) I/O rank step: 1 External libraries for partitioning: METIS Reading metadata from file: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: IN THE DATA SPECIFICATION @ ======== @ @ The pseudo coupling of turbulent dissipation and turbulent @ kinetic energy (ikecou = 1) is not compatible with the use @ of fluid/solid option to disable the dynamic in the solid @ cells (fluid_solid =1). @ @ The parameter ikecou is forced to 0 (no coupling) @ @ The calculation will be run. @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 5 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 1 (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 TempC 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** 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 = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) ------------------------------------------------------------- Variable Number ISCACP ITURT VISLS0 SIGMAS ------------------------------------------------------------- TempC 1 1 0 0.2000E+00 0.1000E+01 ------------------------------------------------------------- ------------------------------------ Variable Number RVARFL ------------------------------------ TempC 1 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempC 1 -1 -0.1000E+13 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. ISCACP = 0 or 1 2 (use Cp or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 or 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS THETVS ------------------------------------------------------ 1 0.0000E+00 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 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 = 50 (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 = 7 (Force exerted by the fluid on the boundary) ipstyp = 1 (y+ at boundary) ipsttp = 1 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 1 (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: MED 3.2.1 options: time dependency: fixed mesh output: every 20 time steps -5: name: directory: monitoring format: time_plot options: time dependency: fixed mesh output: every 1 time steps -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at calculation end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at calculation end Reading file: mesh_input Finished reading: mesh_input No "partition_input/domain_number_2" file available; ---------------------------------------------------------- Partitioning by space-filling curve: Morton (in bounding box). Number of cells per domain (histogramm): [ 5000 ; 5000 ] = 2 Partitioning finished (0.054 s) Before insertion of user-defined boundary Number of cells: 10000 Number of interior faces: 19800 Number of boundary faces: 20400 Number of vertices: 20402 After insertion of user-defined boundary Number of cells: 10000 Number of interior faces: 19600 Number of boundary faces: 20800 Number of vertices: 20806 ---------------------------------------------------------- Halo construction with standard neighborhood ============================================ Face interfaces creation Vertex interfaces creation Halo creation Halo definition Local halo definition Distant halo creation Updating the faces -> cells connectivity Histogram of the number of cells per rank: minimum value = 5000 maximum value = 5000 1 : [ 5000 ; 5000 ] = 2 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 5100 maximum value = 5100 1 : [ 5100 ; 5100 ] = 2 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 100 maximum value = 100 1 : [ 100 ; 100 ] = 2 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 9850 maximum value = 9850 1 : [ 9850 ; 9850 ] = 2 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 10400 maximum value = 10400 1 : [ 10400 ; 10400 ] = 2 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 1 : [ 2 ; 3 [ = 12 2 : [ 3 ; 4 ] = 9988 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 1 maximum value = 1 1 : [ 1 ; 1 ] = 2 ---------------------------------------------------------- Global definition of the number of elements (cells, vertices, faces...) Synchronizing cell families Writing file: mesh_output Finished writing: mesh_output Renumbering mesh: renumbering for cells: pre-numbering: no renumbering cells adjacent to ghost cells last: no numbering: no renumbering renumbering for interior faces: cell adjacency pre-ordering: lowest id first faces adjacent to ghost cells last: no numbering: multipass renumbering for boundary faces: numbering: no shared cell across threads renumbering for vertices: numbering: no renumbering Numbering for cells: type: default Numbering for interior faces: type: default Numbering for boundary faces: type: default ---------------------------------------------------------- Histogram of volume mesh matrix bandwidth per rank: minimum value = 4951 maximum value = 5000 1 : [ 4951 ; 4960 [ = 1 2 : [ 4960 ; 4970 [ = 0 3 : [ 4970 ; 4980 [ = 0 4 : [ 4980 ; 4990 [ = 0 5 : [ 4990 ; 5000 ] = 1 Histogram of volume mesh matrix profile/lines per rank: minimum value = 99 maximum value = 100 1 : [ 99 ; 100 ] = 2 Mesh coordinates: minimum and maximum X : 0.0000000e+00 1.0000000e+00 Y : 0.0000000e+00 1.0000000e+00 Z : 0.0000000e+00 1.0000000e-02 Mesh Number of cells: 10000 Number of interior faces: 19600 Number of boundary faces: 20800 Number of vertices: 20806 Groups: "auto:internal_coupling_0" boundary faces: 400 --- Information on the volumes Minimum control volume = 1.0000000e-06 Maximum control volume = 1.0000000e-06 Total volume for the domain = 1.0000000e-02 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 (0.00794 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 10000 Volume = 1.0000000e-02 Surface = -1 (not computed) Volume zone "all_cells" id = 1 Number of cells = 10000 Volume = 1.0000000e-02 Surface = -1 (not computed) --- Information on boundary zones Boundary zone "boundary_faces" id = 0 Number of faces = 20800 Surface = 2.0800000e+00 Perimeter = -1 (not computed) Boundary zone "BC_1" id = 1 Number of faces = 20800 Surface = 2.0800000e+00 Perimeter = -1 (not computed) Internal coupling coupling_id = 0 Coupled scalar: temperature Cell group selection criterion: x<0.25001 or x>0.74999 Face group selection criterion: auto:internal_coupling_0 Locator: n dist points (total coupled boundary faces) = 400 ALMAX = 0.21544E+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 TempC 0.0000E+00 0.0000E+00 --------------------------------- dt 0.5000E-01 0.5000E-01 --------------------------------- ------------------------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 0 Smooth wall 5 20800 Rough wall 6 0 Symmetry 4 0 Free outlet 3 0 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.500000000E-01 TIME STEP NUMBER 1 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1000E+01 0.1000E+03 molecular_viscos 0.1830E-04 0.1830E-04 specific_heat 0.1017E+04 0.1017E+04 ----------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TempC 1 0.2000E+00 0.1000E+01 ----------------------------------------------- ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.93074E-13 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97020E-03 2 0.70562E+02 0.37610E-03 0.20000E+02 c Velocity[X] 0.73550E-05 c Velocity[Y] 0.36874E-03 c Velocity[Z] 0.55554E-37 c Pressure 0.34284E-02 2 0.50010E+00 0.10000E+01 0.20000E+02 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.060643 0 -6.0643e-06 -6.0643e-06 v Velocity[Y] 0 0.42389 0.00052642 0.00052642 v Velocity[Z] 0 5.2704e-18 5.2704e-22 5.2704e-22 v ǁVelocityǁ 0 0.42821 0.00052686 0.00052686 v Pressure -2.4279 0.0026462 -1.6254e-17 -1.6538e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0 0 0 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 0 0 0 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.0366 0.018204 0.018204 INSTANT 0.100000000E+00 TIME STEP NUMBER 2 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.39588E-02 Friction velocity uk : 0.00000E+00 0.39588E-02 Dimensionless distance yplus : 0.00000E+00 0.10817E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.20135E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18220E-02 2 0.37580E+02 0.24665E-04 0.42021E+01 c Velocity[X] 0.37678E-05 c Velocity[Y] 0.20897E-04 c Velocity[Z] 0.28483E-37 c Pressure 0.38853E-02 2 0.55203E+00 0.10000E+01 0.20000E+02 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.10405 0 -1.0409e-05 -1.0409e-05 v Velocity[Y] 0 0.49979 0.0010181 0.0010181 v Velocity[Z] 0 9.0442e-18 9.0482e-22 9.0482e-22 v ǁVelocityǁ 0 0.5105 0.0010192 0.0010192 v Pressure -2.6555 0.0032468 -1.7852e-17 -1.7936e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.61066 0.0025173 0.0025173 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 108.17 2.5885 2.5885 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.61093 0.020721 0.020721 INSTANT 0.150000000E+00 TIME STEP NUMBER 3 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43225E-02 Friction velocity uk : 0.00000E+00 0.43225E-02 Dimensionless distance yplus : 0.00000E+00 0.11810E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.21984E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18682E-02 2 0.36654E+02 0.10166E-04 0.25123E+01 c Velocity[X] 0.19939E-07 c Velocity[Y] 0.10146E-04 c Velocity[Z] 0.13671E-39 c Pressure 0.22245E-02 2 0.91081E+00 0.91623E+00 0.11600E+01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.10089 0 -1.0108e-05 -1.0108e-05 v Velocity[Y] 0 0.51939 0.0015042 0.0015042 v Velocity[Z] 0 8.7831e-18 8.7998e-22 8.7998e-22 v ǁVelocityǁ 0 0.5291 0.0015052 0.0015052 v Pressure -2.819 0.0063012 2.6001e-17 2.6343e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.76642 0.0049436 0.0049436 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 118.1 3.6556 3.6556 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.76669 0.023148 0.023148 INSTANT 0.200000000E+00 TIME STEP NUMBER 4 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44006E-02 Friction velocity uk : 0.00000E+00 0.44006E-02 Dimensionless distance yplus : 0.00000E+00 0.12023E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22381E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18988E-02 2 0.36062E+02 0.94485E-05 0.22924E+01 c Velocity[X] 0.19904E-07 c Velocity[Y] 0.94286E-05 c Velocity[Z] 0.13448E-39 c Pressure 0.22374E-02 2 0.92348E+00 0.92624E+00 0.46206E+00 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.097741 0 -9.8082e-06 -9.8082e-06 v Velocity[Y] 0 0.52443 0.0019888 0.0019888 v Velocity[Z] 0 8.5241e-18 8.5538e-22 8.5538e-22 v ǁVelocityǁ 0 0.53346 0.0019897 0.0019897 v Pressure -2.8855 0.0093299 -3.3795e-17 -3.439e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.79264 0.0073442 0.0073442 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.23 4.4732 4.4732 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.79291 0.025548 0.025548 INSTANT 0.250000000E+00 TIME STEP NUMBER 5 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44187E-02 Friction velocity uk : 0.00000E+00 0.44187E-02 Dimensionless distance yplus : 0.00000E+00 0.12073E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22473E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.19048E-02 2 0.35950E+02 0.93916E-05 0.21579E+01 c Velocity[X] 0.68310E-08 c Velocity[Y] 0.93847E-05 c Velocity[Z] 0.41967E-40 c Pressure 0.22537E-02 2 0.92797E+00 0.93044E+00 0.25243E+00 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095899 0 -9.6388e-06 -9.6388e-06 v Velocity[Y] 0 0.52628 0.0024731 0.0024731 v Velocity[Z] 0 8.3798e-18 8.4224e-22 8.4224e-22 v ǁVelocityǁ 0 0.53494 0.002474 0.002474 v Pressure -2.9221 0.01233 1.3012e-17 1.2896e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.80067 0.0097411 0.0097411 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.73 5.1622 5.1622 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.80095 0.027945 0.027945 INSTANT 0.300000000E+00 TIME STEP NUMBER 6 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44248E-02 Friction velocity uk : 0.00000E+00 0.44248E-02 Dimensionless distance yplus : 0.00000E+00 0.12090E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22505E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.19061E-02 2 0.35924E+02 0.93809E-05 0.20294E+01 c Velocity[X] 0.19612E-08 c Velocity[Y] 0.93790E-05 c Velocity[Z] 0.97922E-41 c Pressure 0.22738E-02 2 0.93092E+00 0.93334E+00 0.16275E+00 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.09492 0 -9.5556e-06 -9.5556e-06 v Velocity[Y] 0 0.52703 0.0029573 0.0029573 v Velocity[Z] 0 8.3111e-18 8.3665e-22 8.3665e-22 v ǁVelocityǁ 0 0.53551 0.0029581 0.0029581 v Pressure -2.9456 0.015303 3.5305e-18 3.3246e-18 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.80637 0.012137 0.012137 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.9 5.7692 5.7692 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.80664 0.030341 0.030341 INSTANT 0.350000000E+00 TIME STEP NUMBER 7 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44271E-02 Friction velocity uk : 0.00000E+00 0.44271E-02 Dimensionless distance yplus : 0.00000E+00 0.12096E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22516E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.19061E-02 2 0.35924E+02 0.93785E-05 0.19054E+01 c Velocity[X] 0.54328E-09 c Velocity[Y] 0.93779E-05 c Velocity[Z] 0.17751E-41 c Pressure 0.22977E-02 2 0.93345E+00 0.93584E+00 0.11869E+00 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094419 0 -9.5202e-06 -9.5202e-06 v Velocity[Y] 0 0.52727 0.0034414 0.0034414 v Velocity[Z] 0 8.2842e-18 8.3524e-22 8.3524e-22 v ǁVelocityǁ 0 0.53566 0.0034423 0.0034423 v Pressure -2.9626 0.018248 4.1744e-17 4.1674e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.81176 0.014534 0.014534 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.96 6.318 6.318 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.81204 0.032738 0.032738 INSTANT 0.400000000E+00 TIME STEP NUMBER 8 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44278E-02 Friction velocity uk : 0.00000E+00 0.44278E-02 Dimensionless distance yplus : 0.00000E+00 0.12098E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22520E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.19056E-02 2 0.35935E+02 0.93780E-05 0.17876E+01 c Velocity[X] 0.16125E-09 c Velocity[Y] 0.93778E-05 c Velocity[Z] 0.36943E-42 c Pressure 0.23255E-02 2 0.93586E+00 0.93821E+00 0.96260E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094176 0 -9.5105e-06 -9.5105e-06 v Velocity[Y] 0 0.52726 0.0039255 0.0039255 v Velocity[Z] 0 8.2797e-18 8.3608e-22 8.3608e-22 v ǁVelocityǁ 0 0.5356 0.0039264 0.0039264 v Pressure -2.9761 0.021167 -4.4609e-17 -4.5041e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.81712 0.01693 0.01693 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.98 6.8226 6.8226 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.81739 0.035134 0.035134 INSTANT 0.450000000E+00 TIME STEP NUMBER 9 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44275E-02 Friction velocity uk : 0.00000E+00 0.44275E-02 Dimensionless distance yplus : 0.00000E+00 0.12097E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22518E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.19047E-02 2 0.35950E+02 0.93779E-05 0.16776E+01 c Velocity[X] 0.65595E-10 c Velocity[Y] 0.93778E-05 c Velocity[Z] 0.44136E-42 c Pressure 0.23568E-02 2 0.93824E+00 0.94055E+00 0.84762E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094069 0 -9.5145e-06 -9.5145e-06 v Velocity[Y] 0 0.52711 0.0044096 0.0044096 v Velocity[Z] 0 8.2871e-18 8.3812e-22 8.3812e-22 v ǁVelocityǁ 0 0.53544 0.0044105 0.0044105 v Pressure -2.9879 0.024059 6.1884e-17 6.1558e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.82246 0.019326 0.019326 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.97 7.2923 7.2923 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.82274 0.03753 0.03753 INSTANT 0.500000000E+00 TIME STEP NUMBER 10 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44269E-02 Friction velocity uk : 0.00000E+00 0.44269E-02 Dimensionless distance yplus : 0.00000E+00 0.12095E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22515E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.19038E-02 2 0.35969E+02 0.93779E-05 0.15758E+01 c Velocity[X] 0.45128E-10 c Velocity[Y] 0.93778E-05 c Velocity[Z] 0.70792E-42 c Pressure 0.23916E-02 2 0.94063E+00 0.94289E+00 0.78876E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094035 0 -9.5257e-06 -9.5257e-06 v Velocity[Y] 0 0.52689 0.0048937 0.0048937 v Velocity[Z] 0 8.3009e-18 8.4078e-22 8.4078e-22 v ǁVelocityǁ 0 0.53522 0.0048946 0.0048946 v Pressure -2.9987 0.026924 1.2346e-17 1.1308e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.82781 0.021722 0.021722 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.95 7.7335 7.7335 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.82808 0.039926 0.039926 INSTANT 0.550000000E+00 TIME STEP NUMBER 11 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44259E-02 Friction velocity uk : 0.00000E+00 0.44259E-02 Dimensionless distance yplus : 0.00000E+00 0.12093E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22510E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.19027E-02 2 0.35988E+02 0.93779E-05 0.14824E+01 c Velocity[X] 0.42795E-10 c Velocity[Y] 0.93778E-05 c Velocity[Z] 0.91126E-42 c Pressure 0.24298E-02 2 0.94304E+00 0.94524E+00 0.75895E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094038 0 -9.5407e-06 -9.5407e-06 v Velocity[Y] 0 0.52664 0.0053778 0.0053778 v Velocity[Z] 0 8.3179e-18 8.4377e-22 8.4377e-22 v ǁVelocityǁ 0 0.53497 0.0053787 0.0053787 v Pressure -3.0091 0.029763 3.4173e-17 3.2865e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.83315 0.024118 0.024118 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.93 8.1508 8.1508 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.83342 0.042322 0.042322 INSTANT 0.600000000E+00 TIME STEP NUMBER 12 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44249E-02 Friction velocity uk : 0.00000E+00 0.44249E-02 Dimensionless distance yplus : 0.00000E+00 0.12090E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22505E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 12, Physical time 0.60000E+00 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 12: 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 0.19016E-02 2 0.36009E+02 0.93779E-05 0.13970E+01 c Velocity[X] 0.43959E-10 c Velocity[Y] 0.93778E-05 c Velocity[Z] 0.10345E-41 c Pressure 0.24711E-02 2 0.94546E+00 0.94760E+00 0.74431E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094063 0 -9.5577e-06 -9.5577e-06 v Velocity[Y] 0 0.52637 0.0058619 0.0058619 v Velocity[Z] 0 8.3365e-18 8.4694e-22 8.4694e-22 v ǁVelocityǁ 0 0.53471 0.0058627 0.0058627 v Pressure -3.0191 0.032576 2.3603e-17 2.2997e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.83849 0.026514 0.026514 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.9 8.5476 8.5476 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.83876 0.044718 0.044718 INSTANT 0.650000000E+00 TIME STEP NUMBER 13 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44238E-02 Friction velocity uk : 0.00000E+00 0.44238E-02 Dimensionless distance yplus : 0.00000E+00 0.12087E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22500E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.19005E-02 2 0.36030E+02 0.93779E-05 0.13190E+01 c Velocity[X] 0.45261E-10 c Velocity[Y] 0.93778E-05 c Velocity[Z] 0.11023E-41 c Pressure 0.25154E-02 2 0.94787E+00 0.94995E+00 0.73766E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094097 0 -9.5759e-06 -9.5759e-06 v Velocity[Y] 0 0.52609 0.006346 0.006346 v Velocity[Z] 0 8.3561e-18 8.5019e-22 8.5019e-22 v ǁVelocityǁ 0 0.53444 0.0063468 0.0063468 v Pressure -3.0291 0.035363 2.5135e-17 2.5835e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.84382 0.02891 0.02891 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.87 8.9268 8.9268 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.8441 0.047114 0.047114 INSTANT 0.700000000E+00 TIME STEP NUMBER 14 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44227E-02 Friction velocity uk : 0.00000E+00 0.44227E-02 Dimensionless distance yplus : 0.00000E+00 0.12084E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18994E-02 2 0.36051E+02 0.93778E-05 0.12479E+01 c Velocity[X] 0.46156E-10 c Velocity[Y] 0.93778E-05 c Velocity[Z] 0.11372E-41 c Pressure 0.25626E-02 2 0.95026E+00 0.95228E+00 0.73529E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094138 0 -9.5946e-06 -9.5946e-06 v Velocity[Y] 0 0.52581 0.0068301 0.0068301 v Velocity[Z] 0 8.3761e-18 8.535e-22 8.535e-22 v ǁVelocityǁ 0 0.53417 0.0068309 0.0068309 v Pressure -3.0391 0.038124 -4.7029e-17 -4.8239e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.84916 0.031306 0.031306 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.84 9.2905 9.2905 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.84943 0.04951 0.04951 INSTANT 0.750000000E+00 TIME STEP NUMBER 15 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44216E-02 Friction velocity uk : 0.00000E+00 0.44216E-02 Dimensionless distance yplus : 0.00000E+00 0.12081E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22488E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18983E-02 2 0.36072E+02 0.93778E-05 0.11831E+01 c Velocity[X] 0.46700E-10 c Velocity[Y] 0.93778E-05 c Velocity[Z] 0.11538E-41 c Pressure 0.26124E-02 2 0.95262E+00 0.95458E+00 0.73523E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094181 0 -9.6136e-06 -9.6136e-06 v Velocity[Y] 0 0.52552 0.0073141 0.0073141 v Velocity[Z] 0 8.3963e-18 8.5682e-22 8.5682e-22 v ǁVelocityǁ 0 0.5339 0.007315 0.007315 v Pressure -3.049 0.040859 3.5527e-17 3.4495e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.85449 0.033702 0.033702 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.81 9.6405 9.6405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.85477 0.051906 0.051906 INSTANT 0.800000000E+00 TIME STEP NUMBER 16 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44205E-02 Friction velocity uk : 0.00000E+00 0.44205E-02 Dimensionless distance yplus : 0.00000E+00 0.12078E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22483E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18972E-02 2 0.36093E+02 0.93778E-05 0.11238E+01 c Velocity[X] 0.47022E-10 c Velocity[Y] 0.93777E-05 c Velocity[Z] 0.11603E-41 c Pressure 0.26647E-02 2 0.95493E+00 0.95683E+00 0.73646E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094226 0 -9.6328e-06 -9.6328e-06 v Velocity[Y] 0 0.52524 0.0077982 0.0077982 v Velocity[Z] 0 8.4165e-18 8.6016e-22 8.6016e-22 v ǁVelocityǁ 0 0.53363 0.0077991 0.0077991 v Pressure -3.0589 0.043568 3.082e-17 3.026e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.85982 0.036098 0.036098 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.78 9.9782 9.9782 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.8601 0.054302 0.054302 INSTANT 0.850000000E+00 TIME STEP NUMBER 17 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44194E-02 Friction velocity uk : 0.00000E+00 0.44194E-02 Dimensionless distance yplus : 0.00000E+00 0.12075E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22477E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18961E-02 2 0.36113E+02 0.93778E-05 0.10696E+01 c Velocity[X] 0.47215E-10 c Velocity[Y] 0.93777E-05 c Velocity[Z] 0.11616E-41 c Pressure 0.27193E-02 2 0.95719E+00 0.95903E+00 0.73844E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094272 0 -9.6521e-06 -9.6521e-06 v Velocity[Y] 0 0.52496 0.0082823 0.0082823 v Velocity[Z] 0 8.4367e-18 8.6349e-22 8.6349e-22 v ǁVelocityǁ 0 0.53336 0.0082832 0.0082832 v Pressure -3.0689 0.046252 -6.2661e-17 -6.3104e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.86515 0.038493 0.038493 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.75 10.305 10.305 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.86542 0.056697 0.056697 INSTANT 0.900000000E+00 TIME STEP NUMBER 18 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44183E-02 Friction velocity uk : 0.00000E+00 0.44183E-02 Dimensionless distance yplus : 0.00000E+00 0.12072E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22471E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18950E-02 2 0.36134E+02 0.93777E-05 0.10198E+01 c Velocity[X] 0.47337E-10 c Velocity[Y] 0.93777E-05 c Velocity[Z] 0.11601E-41 c Pressure 0.27762E-02 2 0.95937E+00 0.96116E+00 0.74088E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094318 0 -9.6715e-06 -9.6715e-06 v Velocity[Y] 0 0.52469 0.0087664 0.0087664 v Velocity[Z] 0 8.4569e-18 8.6683e-22 8.6683e-22 v ǁVelocityǁ 0 0.5331 0.0087672 0.0087672 v Pressure -3.0788 0.048909 -3.717e-17 -3.8604e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.87048 0.040889 0.040889 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.72 10.621 10.621 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.87075 0.059093 0.059093 INSTANT 0.950000000E+00 TIME STEP NUMBER 19 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44172E-02 Friction velocity uk : 0.00000E+00 0.44172E-02 Dimensionless distance yplus : 0.00000E+00 0.12069E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22466E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18939E-02 2 0.36155E+02 0.93777E-05 0.97412E+00 c Velocity[X] 0.47421E-10 c Velocity[Y] 0.93777E-05 c Velocity[Z] 0.11572E-41 c Pressure 0.28351E-02 2 0.96149E+00 0.96322E+00 0.74362E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094364 0 -9.6909e-06 -9.6909e-06 v Velocity[Y] 0 0.52441 0.0092505 0.0092505 v Velocity[Z] 0 8.477e-18 8.7017e-22 8.7017e-22 v ǁVelocityǁ 0 0.53284 0.0092513 0.0092513 v Pressure -3.0888 0.051541 6.2705e-17 6.1791e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.8758 0.043285 0.043285 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.69 10.929 10.929 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.87607 0.061489 0.061489 INSTANT 0.100000000E+01 TIME STEP NUMBER 20 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44161E-02 Friction velocity uk : 0.00000E+00 0.44161E-02 Dimensionless distance yplus : 0.00000E+00 0.12066E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22460E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18928E-02 2 0.36176E+02 0.93777E-05 0.93202E+00 c Velocity[X] 0.47484E-10 c Velocity[Y] 0.93776E-05 c Velocity[Z] 0.11535E-41 c Pressure 0.28959E-02 2 0.96352E+00 0.96521E+00 0.74658E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.09441 0 -9.7103e-06 -9.7103e-06 v Velocity[Y] 0 0.52414 0.0097345 0.0097345 v Velocity[Z] 0 8.4971e-18 8.735e-22 8.735e-22 v ǁVelocityǁ 0 0.53258 0.0097354 0.0097354 v Pressure -3.0989 0.054148 -2.9843e-17 -3.0451e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.88112 0.04568 0.04568 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.66 11.228 11.228 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.88139 0.063884 0.063884 INSTANT 0.105000000E+01 TIME STEP NUMBER 21 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44150E-02 Friction velocity uk : 0.00000E+00 0.44150E-02 Dimensionless distance yplus : 0.00000E+00 0.12063E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22455E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18918E-02 2 0.36196E+02 0.93776E-05 0.89316E+00 c Velocity[X] 0.47536E-10 c Velocity[Y] 0.93776E-05 c Velocity[Z] 0.11495E-41 c Pressure 0.29586E-02 2 0.96547E+00 0.96711E+00 0.74972E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094457 0 -9.7297e-06 -9.7297e-06 v Velocity[Y] 0 0.52388 0.010219 0.010219 v Velocity[Z] 0 8.517e-18 8.7683e-22 8.7683e-22 v ǁVelocityǁ 0 0.53232 0.010219 0.010219 v Pressure -3.1089 0.056729 8.1268e-18 6.3316e-18 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.88644 0.048076 0.048076 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.63 11.519 11.519 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.88671 0.06628 0.06628 INSTANT 0.110000000E+01 TIME STEP NUMBER 22 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44140E-02 Friction velocity uk : 0.00000E+00 0.44140E-02 Dimensionless distance yplus : 0.00000E+00 0.12060E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22449E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18907E-02 2 0.36217E+02 0.93776E-05 0.85720E+00 c Velocity[X] 0.47582E-10 c Velocity[Y] 0.93776E-05 c Velocity[Z] 0.11453E-41 c Pressure 0.30229E-02 2 0.96734E+00 0.96894E+00 0.75300E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094503 0 -9.7492e-06 -9.7492e-06 v Velocity[Y] 0 0.52361 0.010703 0.010703 v Velocity[Z] 0 8.537e-18 8.8016e-22 8.8016e-22 v ǁVelocityǁ 0 0.53207 0.010704 0.010704 v Pressure -3.119 0.059285 2.8444e-17 2.6194e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.89176 0.050471 0.050471 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.6 11.803 11.803 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.89203 0.068675 0.068675 INSTANT 0.115000000E+01 TIME STEP NUMBER 23 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44129E-02 Friction velocity uk : 0.00000E+00 0.44129E-02 Dimensionless distance yplus : 0.00000E+00 0.12057E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22444E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18896E-02 2 0.36237E+02 0.93776E-05 0.82387E+00 c Velocity[X] 0.47625E-10 c Velocity[Y] 0.93775E-05 c Velocity[Z] 0.11410E-41 c Pressure 0.30888E-02 2 0.96912E+00 0.97067E+00 0.75642E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.09455 0 -9.7686e-06 -9.7686e-06 v Velocity[Y] 0 0.52335 0.011187 0.011187 v Velocity[Z] 0 8.5568e-18 8.8348e-22 8.8348e-22 v ǁVelocityǁ 0 0.53182 0.011188 0.011188 v Pressure -3.1291 0.061816 -4.2588e-17 -4.377e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.89707 0.052867 0.052867 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.57 12.08 12.08 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.89735 0.071071 0.071071 INSTANT 0.120000000E+01 TIME STEP NUMBER 24 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44119E-02 Friction velocity uk : 0.00000E+00 0.44119E-02 Dimensionless distance yplus : 0.00000E+00 0.12054E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22439E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 24, Physical time 0.12000E+01 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 24: 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 0.18886E-02 2 0.36257E+02 0.93776E-05 0.79289E+00 c Velocity[X] 0.47666E-10 c Velocity[Y] 0.93775E-05 c Velocity[Z] 0.11367E-41 c Pressure 0.31561E-02 2 0.97081E+00 0.97233E+00 0.75996E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094596 0 -9.7881e-06 -9.7881e-06 v Velocity[Y] 0 0.52309 0.011671 0.011671 v Velocity[Z] 0 8.5765e-18 8.868e-22 8.868e-22 v ǁVelocityǁ 0 0.53157 0.011672 0.011672 v Pressure -3.1392 0.064321 -4.5675e-17 -4.7836e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.90239 0.055262 0.055262 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.54 12.351 12.351 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.90266 0.073466 0.073466 INSTANT 0.125000000E+01 TIME STEP NUMBER 25 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44108E-02 Friction velocity uk : 0.00000E+00 0.44108E-02 Dimensionless distance yplus : 0.00000E+00 0.12051E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22434E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18875E-02 2 0.36278E+02 0.93775E-05 0.76405E+00 c Velocity[X] 0.47706E-10 c Velocity[Y] 0.93775E-05 c Velocity[Z] 0.11325E-41 c Pressure 0.32248E-02 2 0.97243E+00 0.97391E+00 0.76361E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094642 0 -9.8076e-06 -9.8076e-06 v Velocity[Y] 0 0.52283 0.012155 0.012155 v Velocity[Z] 0 8.5962e-18 8.9012e-22 8.9012e-22 v ǁVelocityǁ 0 0.53133 0.012156 0.012156 v Pressure -3.1494 0.066802 7.7494e-18 5.3363e-18 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.9077 0.057658 0.057658 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.51 12.616 12.616 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.90797 0.075862 0.075862 INSTANT 0.130000000E+01 TIME STEP NUMBER 26 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44098E-02 Friction velocity uk : 0.00000E+00 0.44098E-02 Dimensionless distance yplus : 0.00000E+00 0.12049E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22428E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18864E-02 2 0.36298E+02 0.93775E-05 0.73713E+00 c Velocity[X] 0.47745E-10 c Velocity[Y] 0.93775E-05 c Velocity[Z] 0.11283E-41 c Pressure 0.32948E-02 2 0.97396E+00 0.97540E+00 0.76736E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094688 0 -9.8271e-06 -9.8271e-06 v Velocity[Y] 0 0.52258 0.012639 0.012639 v Velocity[Z] 0 8.6158e-18 8.9344e-22 8.9344e-22 v ǁVelocityǁ 0 0.53109 0.01264 0.01264 v Pressure -3.1596 0.069257 3.5461e-17 3.3161e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.913 0.060053 0.060053 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.49 12.876 12.876 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.91328 0.078257 0.078257 INSTANT 0.135000000E+01 TIME STEP NUMBER 27 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44088E-02 Friction velocity uk : 0.00000E+00 0.44088E-02 Dimensionless distance yplus : 0.00000E+00 0.12046E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22423E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18854E-02 2 0.36318E+02 0.93775E-05 0.71197E+00 c Velocity[X] 0.47784E-10 c Velocity[Y] 0.93774E-05 c Velocity[Z] 0.11241E-41 c Pressure 0.33659E-02 2 0.97541E+00 0.97682E+00 0.77121E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094734 0 -9.8466e-06 -9.8466e-06 v Velocity[Y] 0 0.52233 0.013123 0.013123 v Velocity[Z] 0 8.6354e-18 8.9675e-22 8.9675e-22 v ǁVelocityǁ 0 0.53085 0.013124 0.013124 v Pressure -3.1698 0.071687 -2.9354e-17 -3.2314e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.91831 0.062448 0.062448 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.46 13.131 13.131 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.91859 0.080652 0.080652 INSTANT 0.140000000E+01 TIME STEP NUMBER 28 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44078E-02 Friction velocity uk : 0.00000E+00 0.44078E-02 Dimensionless distance yplus : 0.00000E+00 0.12043E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22418E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18844E-02 2 0.36338E+02 0.93774E-05 0.68841E+00 c Velocity[X] 0.47822E-10 c Velocity[Y] 0.93774E-05 c Velocity[Z] 0.11200E-41 c Pressure 0.34381E-02 2 0.97679E+00 0.97817E+00 0.77515E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094781 0 -9.8661e-06 -9.8661e-06 v Velocity[Y] 0 0.52208 0.013607 0.013607 v Velocity[Z] 0 8.6548e-18 9.0005e-22 9.0005e-22 v ǁVelocityǁ 0 0.53061 0.013608 0.013608 v Pressure -3.1801 0.074093 6.2683e-17 6.0753e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.92362 0.064843 0.064843 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.43 13.38 13.38 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.92389 0.083047 0.083047 INSTANT 0.145000000E+01 TIME STEP NUMBER 29 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44069E-02 Friction velocity uk : 0.00000E+00 0.44069E-02 Dimensionless distance yplus : 0.00000E+00 0.12041E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22413E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18833E-02 2 0.36358E+02 0.93774E-05 0.66630E+00 c Velocity[X] 0.47861E-10 c Velocity[Y] 0.93774E-05 c Velocity[Z] 0.11160E-41 c Pressure 0.35114E-02 2 0.97809E+00 0.97944E+00 0.77918E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094827 0 -9.8857e-06 -9.8857e-06 v Velocity[Y] 0 0.52183 0.014091 0.014091 v Velocity[Z] 0 8.6742e-18 9.0336e-22 9.0336e-22 v ǁVelocityǁ 0 0.53038 0.014092 0.014092 v Pressure -3.1903 0.076474 -5.9397e-17 -6.3252e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.92892 0.067239 0.067239 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.41 13.625 13.625 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.92919 0.085442 0.085442 INSTANT 0.150000000E+01 TIME STEP NUMBER 30 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44059E-02 Friction velocity uk : 0.00000E+00 0.44059E-02 Dimensionless distance yplus : 0.00000E+00 0.12038E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22408E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18823E-02 2 0.36377E+02 0.93774E-05 0.64552E+00 c Velocity[X] 0.47899E-10 c Velocity[Y] 0.93773E-05 c Velocity[Z] 0.11120E-41 c Pressure 0.35856E-02 2 0.97932E+00 0.98065E+00 0.78329E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094873 0 -9.9052e-06 -9.9052e-06 v Velocity[Y] 0 0.52159 0.014575 0.014575 v Velocity[Z] 0 8.6935e-18 9.0666e-22 9.0666e-22 v ǁVelocityǁ 0 0.53015 0.014576 0.014576 v Pressure -3.2006 0.07883 6.5836e-17 6.2638e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.93422 0.069634 0.069634 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.38 13.866 13.866 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.93449 0.087838 0.087838 INSTANT 0.155000000E+01 TIME STEP NUMBER 31 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44049E-02 Friction velocity uk : 0.00000E+00 0.44049E-02 Dimensionless distance yplus : 0.00000E+00 0.12035E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22404E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18813E-02 2 0.36397E+02 0.93774E-05 0.62595E+00 c Velocity[X] 0.47936E-10 c Velocity[Y] 0.93773E-05 c Velocity[Z] 0.11080E-41 c Pressure 0.36606E-02 2 0.98049E+00 0.98178E+00 0.78749E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094919 0 -9.9248e-06 -9.9248e-06 v Velocity[Y] 0 0.52135 0.015059 0.015059 v Velocity[Z] 0 8.7127e-18 9.0996e-22 9.0996e-22 v ǁVelocityǁ 0 0.52992 0.01506 0.01506 v Pressure -3.211 0.081161 5.8442e-17 5.493e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.93952 0.072029 0.072029 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.35 14.103 14.103 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.93979 0.090233 0.090233 INSTANT 0.160000000E+01 TIME STEP NUMBER 32 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44040E-02 Friction velocity uk : 0.00000E+00 0.44040E-02 Dimensionless distance yplus : 0.00000E+00 0.12033E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22399E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18803E-02 2 0.36417E+02 0.93773E-05 0.60750E+00 c Velocity[X] 0.47974E-10 c Velocity[Y] 0.93773E-05 c Velocity[Z] 0.11041E-41 c Pressure 0.37366E-02 2 0.98159E+00 0.98286E+00 0.79175E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.094965 0 -9.9444e-06 -9.9444e-06 v Velocity[Y] 0 0.52112 0.015543 0.015543 v Velocity[Z] 0 8.7319e-18 9.1325e-22 9.1325e-22 v ǁVelocityǁ 0 0.5297 0.015544 0.015544 v Pressure -3.2213 0.083468 6.4126e-17 6.1177e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.94481 0.074424 0.074424 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.33 14.336 14.336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.94509 0.092628 0.092628 INSTANT 0.165000000E+01 TIME STEP NUMBER 33 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44031E-02 Friction velocity uk : 0.00000E+00 0.44031E-02 Dimensionless distance yplus : 0.00000E+00 0.12030E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22394E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18793E-02 2 0.36436E+02 0.93773E-05 0.59008E+00 c Velocity[X] 0.48011E-10 c Velocity[Y] 0.93773E-05 c Velocity[Z] 0.11003E-41 c Pressure 0.38132E-02 2 0.98263E+00 0.98388E+00 0.79608E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.09501 0 -9.964e-06 -9.964e-06 v Velocity[Y] 0 0.52088 0.016028 0.016028 v Velocity[Z] 0 8.751e-18 9.1654e-22 9.1654e-22 v ǁVelocityǁ 0 0.52948 0.016028 0.016028 v Pressure -3.2317 0.085751 6.8834e-18 4.1716e-18 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.95011 0.076819 0.076819 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.3 14.565 14.565 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.95038 0.095023 0.095023 INSTANT 0.170000000E+01 TIME STEP NUMBER 34 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44021E-02 Friction velocity uk : 0.00000E+00 0.44021E-02 Dimensionless distance yplus : 0.00000E+00 0.12028E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22389E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18783E-02 2 0.36456E+02 0.93773E-05 0.57360E+00 c Velocity[X] 0.48048E-10 c Velocity[Y] 0.93772E-05 c Velocity[Z] 0.10965E-41 c Pressure 0.38906E-02 2 0.98361E+00 0.98484E+00 0.80048E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095056 0 -9.9837e-06 -9.9837e-06 v Velocity[Y] 0 0.52065 0.016512 0.016512 v Velocity[Z] 0 8.77e-18 9.1983e-22 9.1983e-22 v ǁVelocityǁ 0 0.52926 0.016513 0.016513 v Pressure -3.2421 0.088009 -4.4986e-17 -4.898e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.9554 0.079214 0.079214 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.28 14.79 14.79 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.95567 0.097417 0.097417 INSTANT 0.175000000E+01 TIME STEP NUMBER 35 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44012E-02 Friction velocity uk : 0.00000E+00 0.44012E-02 Dimensionless distance yplus : 0.00000E+00 0.12025E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22385E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18773E-02 2 0.36475E+02 0.93772E-05 0.55799E+00 c Velocity[X] 0.48085E-10 c Velocity[Y] 0.93772E-05 c Velocity[Z] 0.10927E-41 c Pressure 0.39687E-02 2 0.98453E+00 0.98575E+00 0.80493E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095102 0 -1.0003e-05 -1.0003e-05 v Velocity[Y] 0 0.52042 0.016996 0.016996 v Velocity[Z] 0 8.7889e-18 9.2312e-22 9.2312e-22 v ǁVelocityǁ 0 0.52904 0.016997 0.016997 v Pressure -3.2526 0.090242 -2.8999e-17 -3.2441e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.96069 0.081608 0.081608 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.25 15.012 15.012 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.96096 0.099812 0.099812 INSTANT 0.180000000E+01 TIME STEP NUMBER 36 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.44003E-02 Friction velocity uk : 0.00000E+00 0.44003E-02 Dimensionless distance yplus : 0.00000E+00 0.12023E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22380E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 36, Physical time 0.18000E+01 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 36: 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 0.18763E-02 2 0.36494E+02 0.93772E-05 0.54319E+00 c Velocity[X] 0.48122E-10 c Velocity[Y] 0.93772E-05 c Velocity[Z] 0.10890E-41 c Pressure 0.40474E-02 2 0.98541E+00 0.98660E+00 0.80944E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095148 0 -1.0023e-05 -1.0023e-05 v Velocity[Y] 0 0.5202 0.01748 0.01748 v Velocity[Z] 0 8.8078e-18 9.264e-22 9.264e-22 v ǁVelocityǁ 0 0.52883 0.017481 0.017481 v Pressure -3.263 0.092452 2.6645e-18 -1.4823e-18 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.96597 0.084003 0.084003 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.23 15.231 15.231 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.96625 0.10221 0.10221 INSTANT 0.185000000E+01 TIME STEP NUMBER 37 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43995E-02 Friction velocity uk : 0.00000E+00 0.43995E-02 Dimensionless distance yplus : 0.00000E+00 0.12020E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22376E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18753E-02 2 0.36513E+02 0.93772E-05 0.52914E+00 c Velocity[X] 0.48158E-10 c Velocity[Y] 0.93771E-05 c Velocity[Z] 0.10853E-41 c Pressure 0.41266E-02 2 0.98624E+00 0.98741E+00 0.81400E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095193 0 -1.0043e-05 -1.0043e-05 v Velocity[Y] 0 0.51998 0.017964 0.017964 v Velocity[Z] 0 8.8266e-18 9.2968e-22 9.2968e-22 v ǁVelocityǁ 0 0.52862 0.017965 0.017965 v Pressure -3.2735 0.094637 -4.6452e-17 -5.0737e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.97126 0.086398 0.086398 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.2 15.447 15.447 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.97153 0.1046 0.1046 INSTANT 0.190000000E+01 TIME STEP NUMBER 38 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43986E-02 Friction velocity uk : 0.00000E+00 0.43986E-02 Dimensionless distance yplus : 0.00000E+00 0.12018E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22371E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18743E-02 2 0.36532E+02 0.93772E-05 0.51578E+00 c Velocity[X] 0.48195E-10 c Velocity[Y] 0.93771E-05 c Velocity[Z] 0.10817E-41 c Pressure 0.42064E-02 2 0.98702E+00 0.98818E+00 0.81861E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095239 0 -1.0062e-05 -1.0062e-05 v Velocity[Y] 0 0.51976 0.018448 0.018448 v Velocity[Z] 0 8.8453e-18 9.3296e-22 9.3296e-22 v ǁVelocityǁ 0 0.52841 0.018449 0.018449 v Pressure -3.2841 0.096798 1.3323e-17 9.4232e-18 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.97654 0.088793 0.088793 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.18 15.66 15.66 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.97682 0.107 0.107 INSTANT 0.195000000E+01 TIME STEP NUMBER 39 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43977E-02 Friction velocity uk : 0.00000E+00 0.43977E-02 Dimensionless distance yplus : 0.00000E+00 0.12016E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22367E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18733E-02 2 0.36551E+02 0.93771E-05 0.50307E+00 c Velocity[X] 0.48231E-10 c Velocity[Y] 0.93771E-05 c Velocity[Z] 0.10782E-41 c Pressure 0.42868E-02 2 0.98776E+00 0.98890E+00 0.82327E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095284 0 -1.0082e-05 -1.0082e-05 v Velocity[Y] 0 0.51954 0.018932 0.018932 v Velocity[Z] 0 8.864e-18 9.3624e-22 9.3624e-22 v ǁVelocityǁ 0 0.52821 0.018933 0.018933 v Pressure -3.2946 0.098935 -5.0515e-17 -5.5311e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.98182 0.091187 0.091187 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.16 15.87 15.87 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.9821 0.10939 0.10939 INSTANT 0.200000000E+01 TIME STEP NUMBER 40 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43969E-02 Friction velocity uk : 0.00000E+00 0.43969E-02 Dimensionless distance yplus : 0.00000E+00 0.12013E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22362E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18724E-02 2 0.36570E+02 0.93771E-05 0.49095E+00 c Velocity[X] 0.48267E-10 c Velocity[Y] 0.93771E-05 c Velocity[Z] 0.10747E-41 c Pressure 0.43675E-02 2 0.98845E+00 0.98958E+00 0.82796E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.09533 0 -1.0102e-05 -1.0102e-05 v Velocity[Y] 0 0.51933 0.019416 0.019416 v Velocity[Z] 0 8.8826e-18 9.3951e-22 9.3951e-22 v ǁVelocityǁ 0 0.52801 0.019417 0.019417 v Pressure -3.3052 0.10105 -5.0626e-17 -5.4528e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.9871 0.093582 0.093582 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.13 16.077 16.077 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.98738 0.11179 0.11179 INSTANT 0.205000000E+01 TIME STEP NUMBER 41 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43960E-02 Friction velocity uk : 0.00000E+00 0.43960E-02 Dimensionless distance yplus : 0.00000E+00 0.12011E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22358E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18714E-02 2 0.36589E+02 0.93771E-05 0.47940E+00 c Velocity[X] 0.48303E-10 c Velocity[Y] 0.93770E-05 c Velocity[Z] 0.10712E-41 c Pressure 0.44488E-02 2 0.98911E+00 0.99023E+00 0.83269E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095375 0 -1.0122e-05 -1.0122e-05 v Velocity[Y] 0 0.51912 0.0199 0.0199 v Velocity[Z] 0 8.9011e-18 9.4278e-22 9.4278e-22 v ǁVelocityǁ 0 0.52781 0.019901 0.019901 v Pressure -3.3158 0.10314 -4.6052e-17 -5.1669e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.99238 0.095977 0.095977 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.11 16.282 16.282 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.99265 0.11418 0.11418 INSTANT 0.210000000E+01 TIME STEP NUMBER 42 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43952E-02 Friction velocity uk : 0.00000E+00 0.43952E-02 Dimensionless distance yplus : 0.00000E+00 0.12009E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22354E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18704E-02 2 0.36608E+02 0.93771E-05 0.46837E+00 c Velocity[X] 0.48338E-10 c Velocity[Y] 0.93770E-05 c Velocity[Z] 0.10678E-41 c Pressure 0.45304E-02 2 0.98974E+00 0.99084E+00 0.83745E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095421 0 -1.0141e-05 -1.0141e-05 v Velocity[Y] 0 0.51891 0.020384 0.020384 v Velocity[Z] 0 8.9196e-18 9.4605e-22 9.4605e-22 v ǁVelocityǁ 0 0.52761 0.020385 0.020385 v Pressure -3.3264 0.1052 -3.1353e-17 -3.6909e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 0.99765 0.098371 0.098371 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.09 16.484 16.484 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 0.99793 0.11657 0.11657 INSTANT 0.215000000E+01 TIME STEP NUMBER 43 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43944E-02 Friction velocity uk : 0.00000E+00 0.43944E-02 Dimensionless distance yplus : 0.00000E+00 0.12007E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22350E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18695E-02 2 0.36626E+02 0.93770E-05 0.45782E+00 c Velocity[X] 0.48374E-10 c Velocity[Y] 0.93770E-05 c Velocity[Z] 0.10644E-41 c Pressure 0.46124E-02 2 0.99033E+00 0.99141E+00 0.84224E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095466 0 -1.0161e-05 -1.0161e-05 v Velocity[Y] 0 0.51871 0.020868 0.020868 v Velocity[Z] 0 8.9379e-18 9.4932e-22 9.4932e-22 v ǁVelocityǁ 0 0.52742 0.020869 0.020869 v Pressure -3.3371 0.10724 -4.9316e-17 -5.4655e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 1.0029 0.10077 0.10077 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.07 16.683 16.683 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 1.0032 0.11897 0.11897 INSTANT 0.220000000E+01 TIME STEP NUMBER 44 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43936E-02 Friction velocity uk : 0.00000E+00 0.43936E-02 Dimensionless distance yplus : 0.00000E+00 0.12004E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22346E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18685E-02 2 0.36645E+02 0.93770E-05 0.44773E+00 c Velocity[X] 0.48409E-10 c Velocity[Y] 0.93770E-05 c Velocity[Z] 0.10611E-41 c Pressure 0.46948E-02 2 0.99088E+00 0.99196E+00 0.84706E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095511 0 -1.0181e-05 -1.0181e-05 v Velocity[Y] 0 0.5185 0.021352 0.021352 v Velocity[Z] 0 8.9563e-18 9.5258e-22 9.5258e-22 v ǁVelocityǁ 0 0.52723 0.021353 0.021353 v Pressure -3.3478 0.10926 3.1353e-17 2.6279e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 1.0082 0.10316 0.10316 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.04 16.88 16.88 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 1.0085 0.12136 0.12136 INSTANT 0.225000000E+01 TIME STEP NUMBER 45 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43928E-02 Friction velocity uk : 0.00000E+00 0.43928E-02 Dimensionless distance yplus : 0.00000E+00 0.12002E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22342E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18676E-02 2 0.36663E+02 0.93770E-05 0.43808E+00 c Velocity[X] 0.48445E-10 c Velocity[Y] 0.93769E-05 c Velocity[Z] 0.10579E-41 c Pressure 0.47775E-02 2 0.99141E+00 0.99248E+00 0.85190E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095556 0 -1.0201e-05 -1.0201e-05 v Velocity[Y] 0 0.5183 0.021836 0.021836 v Velocity[Z] 0 8.9745e-18 9.5585e-22 9.5585e-22 v ǁVelocityǁ 0 0.52704 0.021837 0.021837 v Pressure -3.3585 0.11126 4.905e-17 4.1907e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 1.0135 0.10555 0.10555 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120.02 17.075 17.075 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 1.0137 0.12376 0.12376 INSTANT 0.230000000E+01 TIME STEP NUMBER 46 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43920E-02 Friction velocity uk : 0.00000E+00 0.43920E-02 Dimensionless distance yplus : 0.00000E+00 0.12000E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22338E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18667E-02 2 0.36682E+02 0.93770E-05 0.42882E+00 c Velocity[X] 0.48480E-10 c Velocity[Y] 0.93769E-05 c Velocity[Z] 0.10546E-41 c Pressure 0.48606E-02 2 0.99191E+00 0.99297E+00 0.85677E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095601 0 -1.0221e-05 -1.0221e-05 v Velocity[Y] 0 0.51811 0.022321 0.022321 v Velocity[Z] 0 8.9927e-18 9.5911e-22 9.5911e-22 v ǁVelocityǁ 0 0.52686 0.022321 0.022321 v Pressure -3.3693 0.11323 -4.0457e-17 -4.7815e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 1.0187 0.10795 0.10795 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 120 17.268 17.268 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 1.019 0.12615 0.12615 INSTANT 0.235000000E+01 TIME STEP NUMBER 47 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43912E-02 Friction velocity uk : 0.00000E+00 0.43912E-02 Dimensionless distance yplus : 0.00000E+00 0.11998E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22334E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18657E-02 2 0.36700E+02 0.93769E-05 0.41994E+00 c Velocity[X] 0.48515E-10 c Velocity[Y] 0.93769E-05 c Velocity[Z] 0.10514E-41 c Pressure 0.49439E-02 2 0.99238E+00 0.99343E+00 0.86164E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095647 0 -1.024e-05 -1.024e-05 v Velocity[Y] 0 0.51792 0.022805 0.022805 v Velocity[Z] 0 9.0108e-18 9.6237e-22 9.6237e-22 v ǁVelocityǁ 0 0.52667 0.022806 0.022806 v Pressure -3.38 0.11518 2.0184e-17 1.1795e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 1.024 0.11034 0.11034 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 119.98 17.459 17.459 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 1.0243 0.12855 0.12855 INSTANT 0.240000000E+01 TIME STEP NUMBER 48 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43905E-02 Friction velocity uk : 0.00000E+00 0.43905E-02 Dimensionless distance yplus : 0.00000E+00 0.11996E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22330E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 48, Physical time 0.24000E+01 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 48: 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 0.18648E-02 2 0.36718E+02 0.93769E-05 0.41141E+00 c Velocity[X] 0.48550E-10 c Velocity[Y] 0.93769E-05 c Velocity[Z] 0.10483E-41 c Pressure 0.50275E-02 2 0.99283E+00 0.99387E+00 0.86654E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095692 0 -1.026e-05 -1.026e-05 v Velocity[Y] 0 0.51772 0.023289 0.023289 v Velocity[Z] 0 9.0288e-18 9.6562e-22 9.6562e-22 v ǁVelocityǁ 0 0.52649 0.02329 0.02329 v Pressure -3.3908 0.1171 -1.4322e-17 -2.143e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 1.0293 0.11274 0.11274 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 119.96 17.647 17.647 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 1.0295 0.13094 0.13094 INSTANT 0.245000000E+01 TIME STEP NUMBER 49 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43897E-02 Friction velocity uk : 0.00000E+00 0.43897E-02 Dimensionless distance yplus : 0.00000E+00 0.11994E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22326E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.18639E-02 2 0.36736E+02 0.93769E-05 0.40322E+00 c Velocity[X] 0.48584E-10 c Velocity[Y] 0.93768E-05 c Velocity[Z] 0.10452E-41 c Pressure 0.51113E-02 2 0.99326E+00 0.99428E+00 0.87144E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095736 0 -1.028e-05 -1.028e-05 v Velocity[Y] 0 0.51754 0.023773 0.023773 v Velocity[Z] 0 9.0468e-18 9.6888e-22 9.6888e-22 v ǁVelocityǁ 0 0.52632 0.023774 0.023774 v Pressure -3.4017 0.119 -1.0791e-17 -1.7322e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 1.0345 0.11513 0.11513 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 119.94 17.834 17.834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 1.0348 0.13334 0.13334 INSTANT 0.250000000E+01 TIME STEP NUMBER 50 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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 0.43890E-02 Friction velocity uk : 0.00000E+00 0.43890E-02 Dimensionless distance yplus : 0.00000E+00 0.11992E+03 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Rough dim-less th. sca. tplus : 0.18615E-13 0.22322E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write final restart files checkpoint at iteration 50, Physical time 0.25000E+01 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 50: 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 0.18630E-02 2 0.36754E+02 0.93769E-05 0.39535E+00 c Velocity[X] 0.48619E-10 c Velocity[Y] 0.93768E-05 c Velocity[Z] 0.10422E-41 c Pressure 0.51954E-02 2 0.99366E+00 0.99468E+00 0.87635E-01 c TempC 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.095781 0 -1.03e-05 -1.03e-05 v Velocity[Y] 0 0.51735 0.024257 0.024257 v Velocity[Z] 0 9.0647e-18 9.7213e-22 9.7213e-22 v ǁVelocityǁ 0 0.52614 0.024258 0.024258 v Pressure -3.4125 0.12088 4.0035e-17 3.2738e-17 v TempC 0 0 0 0 v Density 1 100 50.5 50.5 v CourantNb 0 1.0398 0.11753 0.11753 v FourierNb 0.000183 0.0366 0.018204 0.018204 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0133e+05 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 0 0 0 0 v Boundary Density 1 100 50.976 50.976 v Yplus 0 119.92 18.018 18.018 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.000183 1.04 0.13573 0.13573 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation