command: .\cs_solver.exe --param setup.xml *************************************************************** (R) Code_Saturne Version 5.0.9 Copyright (C) 1998-2018 EDF S.A., France revision 5.0.9-bcc4a5983-m build 09/26/18 18:46:02 MPI version 2.0 (MS-MPI) 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: 04/16/20 10:53:01 Processor: Directory: E:\CDFtest\hotsquarecavity\RESU\20200416-1052 I/O read method: standard input and output, serial access I/O write method: standard input and output, serial access External libraries for partitioning: SCOTCH 6.0.0 Reading metadata from file: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 5 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 1 (Nb specific physics scalars ) ----------------------------------------------------------- ** VOF METHOD ---------------------------------------- IVOFMT = -1 ( -1: inactive ) ( 0: active ) ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION ---------------------------------------- ICAVIT = -1 (-1: single phase flow ) ( 0: no vap./cond. model ) ( 1: Merkle's model ) ----------------------------------------------------------- ** TIME STEPPING ------------- --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Velocity 1 0.1000E+01 Pressure 0 0.1000E+01 TempK 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 ------ -- Phase continue : 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 ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 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 ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- ------------------------------------ Variable EPSILO IDIRCL ------------------------------------ Velocity 0.1000E-07 1 Pressure 0.1000E-07 1 TempK 0.1000E-07 1 ------------------------------------ EPSILO = (resolution precision) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet) ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) ------------------------------------------------------------- Variable Number ISCACP ITURT VISLS0 SIGMAS ------------------------------------------------------------- TempK 1 1 0 0.2590E-01 0.1000E+01 ------------------------------------------------------------- ------------------------------------ Variable Number RVARFL ------------------------------------ TempK 1 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempK 1 -1 0.0000E+00 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 IVSEXT THETVS ------------------------------------------------------ 1 0.0000E+00 0 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) IVSEXT = (extrap. total viscosity ) (0: explicit ) (1: n+thetvs with thetvs=1/2 ) (2: n+thetvs with thetvs=1 ) 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. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 450 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 0 (Checkpoint frequency ) --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) -- -- -- --- Log files NTLIST = 1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) Velocity 0 Pressure 0 TempK 0 TempK -999 Density -999 Boundary Density -999 CourantNb -999 FourierNb -999 total_pressure -999 Local Time Step -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted by the fluid on the boundary) ipstyp = 0 (y+ at boundary) ipsttp = 0 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 1 (Dimensionless thermal flux at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization iterations) IFLXMW = 0 (ALE mass flux computation 0: thanks to vertices 1: thanks to mesh velocity) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: time dependency: fixed mesh output: at calculation end -5: name: directory: monitoring format: time_plot options: time dependency: fixed mesh output: every 1 time steps -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at calculation end Reading file: mesh_input Finished reading: mesh_input Number of cells: 6400 ---------------------------------------------------------- Number of cells + halo cells: 6400 ---------------------------------------------------------- Number of interior faces: 12640 ---------------------------------------------------------- Number of boundary faces: 13120 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 1 : [ 2 ; 3 [ = 4 2 : [ 3 ; 4 ] = 6396 ---------------------------------------------------------- Renumbering mesh: renumbering for cells: pre-numbering: none cells adjacent to ghost cells last: no numbering: none renumbering for interior faces: cell adjacency pre-ordering: lowest id first faces adjacent to ghost cells last: no numbering: none renumbering for boundary faces: numbering: none ---------------------------------------------------------- Matrix bandwidth for volume mesh : 80 Matrix profile/lines for volume mesh : 80 Mesh coordinates: minimum and maximum X : 0.0000000e+000 1.0000000e+000 Y : 0.0000000e+000 1.0000000e+000 Z : 0.0000000e+000 1.0000000e-002 Mesh Number of cells: 6400 Number of interior faces: 12640 Number of boundary faces: 13120 Number of vertices: 13122 Groups: "adiabatic_walls" boundary faces: 160 "cold_wall" boundary faces: 80 "hot_wall" boundary faces: 80 "symmetry_walls" boundary faces: 12800 --- Information on the volumes Minimum control volume = 1.5625000e-006 Maximum control volume = 1.5625000e-006 Total volume for the domain = 1.0000000e-002 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 (0.00698 s) 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 TempK 0.2931E+03 0.2931E+03 --------------------------------- dt 0.1000E+00 0.1000E+00 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E+00 TIME STEP NUMBER 1 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1000E+01 0.1000E+01 molecular_viscos 0.1830E-04 0.1830E-04 ----------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TempK 1 0.2590E-01 0.2590E-01 ----------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 0 Smooth wall 5 320 Rough wall 6 0 Symmetry 4 12800 Free outlet 3 0 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : -0.14085E+14 0.00000E+00 Rough dim-less th. sca. tplus : 0.70998E-12 0.70998E-12 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.25003E-03 8 0.48813E-03 0.25542E-02 0.90909E+01 c Velocity[X] 0.16753E-06 c Velocity[Y] 0.25540E-02 c Velocity[Z] 0.28765E-28 c Pressure 0.34334E-03 25 0.16800E-07 0.10000E+01 0.90909E+01 c TempK 0.33490E+03 5 0.36437E-06 0.13460E-01 0.11932E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.0021669 0.0021669 2.0636e-012 2.0636e-012 v Velocity[Y] -0.005296 0.10641 0.0026805 0.0026805 v Velocity[Z] -8.5487e-015 9.7698e-015 -1.1817e-017 -1.1817e-017 v ǁVelocityǁ 1.8997e-005 0.10644 0.002946 0.002946 v Pressure -0.98696 0.98696 -5.4179e-016 1.0842e-017 v TempK 293.15 293.49 293.15 293.15 v Density 1 1 1 1 v CourantNb 0 0 0 0 v FourierNb 0.025766 0.051533 0.050889 0.050889 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.11 0.11 0.11 0.11 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.15 303.15 293.21 293.2 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.025766 0.051533 0.050889 0.050889 INSTANT 0.200000000E+00 TIME STEP NUMBER 2 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.88489E-04 0.17287E-01 Friction velocity uk : 0.88489E-04 0.17287E-01 Dimensionless distance yplus : 0.30222E-01 0.59041E+01 Friction thermal sca. tstar : -0.16639E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.21457E-01 0.41918E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.25338E-03 8 0.52275E-03 0.16418E-02 0.38133E+01 c Velocity[X] 0.24820E-06 c Velocity[Y] 0.16416E-02 c Velocity[Z] 0.25453E-28 c Pressure 0.46553E-03 24 0.13621E-07 0.10000E+01 0.82645E+01 c TempK 0.30447E+03 6 0.87810E-06 0.13196E-01 0.11265E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.0057201 0.0057201 -4.4814e-012 -4.4814e-012 v Velocity[Y] -0.029817 0.19311 0.0042103 0.0042103 v Velocity[Z] -1.6845e-014 2.0224e-014 -2.6703e-017 -2.6703e-017 v ǁVelocityǁ 5.744e-006 0.1932 0.005926 0.005926 v Pressure -0.99243 0.99243 -1.3323e-016 4.6621e-016 v TempK 293.15 293.86 293.16 293.16 v Density 1 1 1 1 v CourantNb 5.1782e-005 0.051266 0.0030247 0.0030247 v FourierNb 0.028343 0.056686 0.055978 0.055978 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.121 0.121 0.121 0.121 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.15 303.15 293.22 293.2 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.042566 0.09378 0.059002 0.059002 INSTANT 0.300000000E+00 TIME STEP NUMBER 3 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12990E-03 0.23134E-01 Friction velocity uk : 0.12990E-03 0.23134E-01 Dimensionless distance yplus : 0.44364E-01 0.79010E+01 Friction thermal sca. tstar : -0.73839E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.31498E-01 0.56095E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.44953E-04 8 0.30564E-02 0.13333E-02 0.22980E+01 c Velocity[X] 0.80743E-07 c Velocity[Y] 0.13332E-02 c Velocity[Z] 0.15107E-28 c Pressure 0.73826E-04 12 0.36639E-07 0.13049E+00 0.68755E-02 c TempK 0.27681E+03 6 0.11924E-05 0.12835E-01 0.10592E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.0091531 0.0091531 -1.412e-011 -1.412e-011 v Velocity[Y] -0.058865 0.2732 0.0055424 0.0055424 v Velocity[Z] -2.3354e-014 2.8619e-014 -4.1754e-017 -4.1754e-017 v ǁVelocityǁ 1.1122e-005 0.27335 0.0086979 0.0086979 v Pressure -0.99442 0.99448 -3.4639e-016 2.6021e-016 v TempK 293.15 294.26 293.16 293.16 v Density 1 1 1 1 v CourantNb 0.00012279 0.12212 0.0072193 0.0072193 v FourierNb 0.031177 0.062355 0.061575 0.061575 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.1331 0.1331 0.1331 0.1331 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.15 303.15 293.22 293.21 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.046889 0.16888 0.068795 0.068795 INSTANT 0.400000000E+00 TIME STEP NUMBER 4 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12454E-03 0.27585E-01 Friction velocity uk : 0.12454E-03 0.27585E-01 Dimensionless distance yplus : 0.42536E-01 0.94213E+01 Friction thermal sca. tstar : -0.95224E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.30200E-01 0.66889E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.51929E-04 8 0.35727E-02 0.11425E-02 0.15718E+01 c Velocity[X] 0.25984E-06 c Velocity[Y] 0.11422E-02 c Velocity[Z] 0.12338E-28 c Pressure 0.51648E-04 11 0.10363E-07 0.78571E-01 0.17631E-02 c TempK 0.25167E+03 7 0.23954E-05 0.12356E-01 0.99093E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.016025 0.016025 -8.4235e-011 -8.4235e-011 v Velocity[Y] -0.092838 0.35092 0.0067858 0.0067858 v Velocity[Z] -2.9431e-014 3.6411e-014 -5.735e-017 -5.735e-017 v ǁVelocityǁ 8.9932e-006 0.35129 0.011552 0.011552 v Pressure -0.9952 0.99504 -8.8818e-018 5.9631e-016 v TempK 293.15 294.72 293.17 293.17 v Density 1 1 1 1 v CourantNb 0.00012429 0.13127 0.007651 0.007651 v FourierNb 0.034295 0.06859 0.067733 0.067733 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.14641 0.14641 0.14641 0.14641 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.15 303.15 293.22 293.21 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.051567 0.18271 0.075384 0.075384 INSTANT 0.500000000E+00 TIME STEP NUMBER 5 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11988E-03 0.31067E-01 Friction velocity uk : 0.11988E-03 0.31067E-01 Dimensionless distance yplus : 0.40942E-01 0.10610E+02 Friction thermal sca. tstar : -0.10870E+03 0.00000E+00 Rough dim-less th. sca. tplus : 0.29068E-01 0.75331E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.57705E-04 10 0.59289E-02 0.10093E-02 0.11527E+01 c Velocity[X] 0.10155E-05 c Velocity[Y] 0.10083E-02 c Velocity[Z] 0.98398E-29 c Pressure 0.38593E-04 9 0.79745E-08 0.51642E-01 0.10063E-02 c TempK 0.22881E+03 9 0.69129E-05 0.11828E-01 0.92438E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.030883 0.030883 -1.1654e-011 -1.1654e-011 v Velocity[Y] -0.13353 0.43179 0.0079968 0.0079968 v Velocity[Z] -3.5514e-014 4.3497e-014 -7.2932e-017 -7.2932e-017 v ǁVelocityǁ 6.0451e-005 0.4318 0.014477 0.014477 v Pressure -0.99604 0.99525 3.2863e-016 9.1073e-016 v TempK 293.15 295.23 293.17 293.17 v Density 1 1 1 1 v CourantNb 0.00012659 0.27114 0.0083068 0.0083068 v FourierNb 0.037725 0.075449 0.074506 0.074506 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.16105 0.16105 0.16105 0.16105 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.15 303.15 293.23 293.22 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.056713 0.32772 0.082813 0.082813 INSTANT 0.600000000E+00 TIME STEP NUMBER 6 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11435E-03 0.34042E-01 Friction velocity uk : 0.11435E-03 0.34042E-01 Dimensionless distance yplus : 0.39055E-01 0.11626E+02 Friction thermal sca. tstar : -0.73361E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.27728E-01 0.82544E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.62492E-04 13 0.13472E-01 0.91237E-03 0.88556E+00 c Velocity[X] 0.34512E-05 c Velocity[Y] 0.90892E-03 c Velocity[Z] 0.76502E-29 c Pressure 0.33471E-04 9 0.91117E-08 0.39904E-01 0.76661E-03 c TempK 0.20803E+03 13 0.22521E-04 0.11346E-01 0.86318E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.060204 0.060204 3.3367e-011 3.3367e-011 v Velocity[Y] -0.17792 0.52614 0.0091942 0.0091942 v Velocity[Z] -4.1444e-014 4.9821e-014 -8.8117e-017 -8.8117e-017 v ǁVelocityǁ 5.5049e-005 0.52614 0.017423 0.017423 v Pressure -0.9976 0.99536 -1.2612e-015 -7.2642e-016 v TempK 293.14 295.66 293.18 293.18 v Density 1 1 1 1 v CourantNb 0.00012671 0.60371 0.0094324 0.0094324 v FourierNb 0.041497 0.082994 0.081957 0.081957 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.17716 0.17716 0.17716 0.17716 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.15 303.15 293.24 293.22 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.062372 0.66596 0.091389 0.091389 INSTANT 0.700000000E+00 TIME STEP NUMBER 7 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10640E-03 0.36670E-01 Friction velocity uk : 0.10640E-03 0.36670E-01 Dimensionless distance yplus : 0.36340E-01 0.12524E+02 Friction thermal sca. tstar : -0.68544E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.25801E-01 0.88918E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.66799E-04 19 0.34364E-01 0.85152E-03 0.70905E+00 c Velocity[X] 0.83124E-05 c Velocity[Y] 0.84321E-03 c Velocity[Z] 0.57910E-29 c Pressure 0.40112E-04 10 0.10538E-07 0.42982E-01 0.10470E-02 c TempK 0.18913E+03 18 0.50342E-04 0.10703E-01 0.79934E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.10351 0.10351 1.2079e-010 1.2079e-010 v Velocity[Y] -0.20721 0.64453 0.010374 0.010374 v Velocity[Z] -4.6873e-014 5.5359e-014 -1.0262e-016 -1.0262e-016 v ǁVelocityǁ 1.7062e-005 0.64466 0.020372 0.020372 v Pressure -1.0008 0.99543 -1.0303e-015 -3.9031e-016 v TempK 293.1 295.82 293.19 293.19 v Density 1 1 1 1 v CourantNb 0.00012068 1.2805 0.011696 0.011696 v FourierNb 0.045647 0.091293 0.090152 0.090152 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.19487 0.19487 0.19487 0.19487 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.14 303.15 293.24 293.23 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.066902 1.349 0.10185 0.10185 INSTANT 0.800000000E+00 TIME STEP NUMBER 8 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.91194E-04 0.39045E-01 Friction velocity uk : 0.91194E-04 0.39045E-01 Dimensionless distance yplus : 0.31145E-01 0.13335E+02 Friction thermal sca. tstar : -0.71226E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.22113E-01 0.94677E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71169E-04 28 0.66076E-01 0.84074E-03 0.59567E+00 c Velocity[X] 0.16153E-04 c Velocity[Y] 0.82458E-03 c Velocity[Z] 0.42646E-29 c Pressure 0.57980E-04 10 0.15379E-07 0.56268E-01 0.16454E-02 c TempK 0.17196E+03 21 0.70986E-04 0.98074E-02 0.72955E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14195 0.14195 1.2211e-010 1.2211e-010 v Velocity[Y] -0.27411 0.74462 0.011517 0.011517 v Velocity[Z] -5.1762e-014 6.0117e-014 -1.1619e-016 -1.1619e-016 v ǁVelocityǁ 3.0496e-005 0.74565 0.023358 0.023358 v Pressure -1.0057 0.99548 -2.0428e-016 3.2526e-016 v TempK 292.95 296.3 293.19 293.19 v Density 1 1 1 1 v CourantNb 9.7454e-005 2.1902 0.016206 0.016206 v FourierNb 0.050211 0.10042 0.099168 0.099168 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.21436 0.21436 0.21436 0.21436 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.1 303.15 293.25 293.23 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.058299 2.2655 0.11537 0.11537 INSTANT 0.900000000E+00 TIME STEP NUMBER 9 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.47810E-04 0.41093E-01 Friction velocity uk : 0.47810E-04 0.41093E-01 Dimensionless distance yplus : 0.16329E-01 0.14034E+02 Friction thermal sca. tstar : -0.91338E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.11593E-01 0.99643E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76710E-04 39 0.11468E+00 0.85523E-03 0.51618E+00 c Velocity[X] 0.24040E-04 c Velocity[Y] 0.83118E-03 c Velocity[Z] 0.30580E-29 c Pressure 0.81357E-04 11 0.18574E-07 0.71968E-01 0.19974E-02 c TempK 0.15634E+03 24 0.76205E-04 0.90717E-02 0.66898E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14571 0.14571 2.4205e-010 2.4205e-010 v Velocity[Y] -0.32107 0.72647 0.012611 0.012611 v Velocity[Z] -5.6089e-014 6.4118e-014 -1.2868e-016 -1.2868e-016 v ǁVelocityǁ 3.6983e-006 0.72649 0.02632 0.02632 v Pressure -1.0084 0.99556 2.0428e-016 8.6736e-016 v TempK 292.83 296.8 293.2 293.2 v Density 1 1 1 1 v CourantNb 2.9267e-005 3.9186 0.024842 0.024842 v FourierNb 0.055233 0.11047 0.10908 0.10908 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.23579 0.23579 0.23579 0.23579 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.95 303.15 293.25 293.24 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.056051 4.029 0.13393 0.13393 INSTANT 0.100000000E+01 TIME STEP NUMBER 10 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.94454E-04 0.42885E-01 Friction velocity uk : 0.94454E-04 0.42885E-01 Dimensionless distance yplus : 0.32259E-01 0.14647E+02 Friction thermal sca. tstar : -0.81236E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.22903E-01 0.10399E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80126E-04 46 0.13994E+00 0.84603E-03 0.44662E+00 c Velocity[X] 0.39752E-04 c Velocity[Y] 0.80628E-03 c Velocity[Z] 0.21596E-29 c Pressure 0.94182E-04 16 0.15917E-07 0.76029E-01 0.16547E-02 c TempK 0.14215E+03 23 0.72314E-04 0.86496E-02 0.62282E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.13345 0.13345 -2.6946e-010 -2.6946e-010 v Velocity[Y] -0.30337 0.85846 0.013704 0.013704 v Velocity[Z] -5.9846e-014 6.7409e-014 -1.3987e-016 -1.3987e-016 v ǁVelocityǁ 6.4648e-006 0.85983 0.029027 0.029027 v Pressure -1.0054 0.99574 -7.9048e-016 -1.8431e-016 v TempK 292.77 297.31 293.21 293.21 v Density 1 1 1 1 v CourantNb 0.00012325 5.9909 0.037495 0.037495 v FourierNb 0.060756 0.12151 0.11999 0.11999 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25937 0.25937 0.25937 0.25937 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.83 303.15 293.26 293.25 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091259 6.1124 0.15749 0.15749 INSTANT 0.110000000E+01 TIME STEP NUMBER 11 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.95458E-04 0.43573E-01 Friction velocity uk : 0.95458E-04 0.43573E-01 Dimensionless distance yplus : 0.32602E-01 0.14881E+02 Friction thermal sca. tstar : -0.18258E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.23147E-01 0.10565E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81353E-04 44 0.14561E+00 0.96769E-03 0.42134E+00 c Velocity[X] 0.59632E-04 c Velocity[Y] 0.90806E-03 c Velocity[Z] 0.15686E-29 c Pressure 0.12361E-03 11 0.19454E-07 0.91409E-01 0.19077E-02 c TempK 0.12925E+03 23 0.97994E-04 0.82186E-02 0.57884E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18261 0.18261 2.5031e-010 2.5031e-010 v Velocity[Y] -0.40605 0.96305 0.014751 0.014751 v Velocity[Z] -6.3046e-014 7.0052e-014 -1.4883e-016 -1.4883e-016 v ǁVelocityǁ 5.7658e-006 0.96417 0.031591 0.031591 v Pressure -1.0108 0.99745 -7.4607e-016 -1.7347e-016 v TempK 292.68 297.83 293.21 293.21 v Density 1 1 1 1 v CourantNb 0.0001415 6.3369 0.053685 0.053685 v FourierNb 0.066831 0.13366 0.13199 0.13199 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28531 0.28531 0.28531 0.28531 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.77 303.15 293.27 293.25 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096932 6.4706 0.18568 0.18568 INSTANT 0.120000000E+01 TIME STEP NUMBER 12 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.89181E-04 0.45495E-01 Friction velocity uk : 0.89181E-04 0.45495E-01 Dimensionless distance yplus : 0.30458E-01 0.15538E+02 Friction thermal sca. tstar : -0.20843E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.21625E-01 0.11032E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94691E-04 53 0.20223E+00 0.14732E-02 0.46592E+00 c Velocity[X] 0.77862E-04 c Velocity[Y] 0.13954E-02 c Velocity[Z] 0.14304E-29 c Pressure 0.19900E-03 12 0.27677E-07 0.13627E+00 0.24100E-02 c TempK 0.11752E+03 25 0.10318E-03 0.74684E-02 0.52610E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.29278 0.29278 3.1622e-010 3.1622e-010 v Velocity[Y] -0.48674 0.95632 0.015645 0.015645 v Velocity[Z] -6.5716e-014 7.2119e-014 -1.5598e-016 -1.5598e-016 v ǁVelocityǁ 4.0402e-006 0.95661 0.033895 0.033895 v Pressure -1.0155 0.99891 -9.2371e-016 -3.7947e-016 v TempK 292.74 297.89 293.22 293.22 v Density 1 1 1 1 v CourantNb 0.00013285 6.7127 0.084751 0.084751 v FourierNb 0.073515 0.14703 0.14519 0.14519 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31384 0.31384 0.31384 0.31384 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.68 303.15 293.27 293.26 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1104 6.8598 0.22994 0.22994 INSTANT 0.130000000E+01 TIME STEP NUMBER 13 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13425E-04 0.41537E-01 Friction velocity uk : 0.13425E-04 0.41537E-01 Dimensionless distance yplus : 0.45850E-02 0.14186E+02 Friction thermal sca. tstar : -0.32802E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.32553E-02 0.10072E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10112E-03 58 0.23302E+00 0.17766E-02 0.46333E+00 c Velocity[X] 0.13364E-03 c Velocity[Y] 0.16430E-02 c Velocity[Z] 0.15776E-29 c Pressure 0.24789E-03 12 0.30237E-07 0.15752E+00 0.24086E-02 c TempK 0.10687E+03 24 0.16588E-03 0.71443E-02 0.49060E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23716 0.23717 7.9312e-010 7.9312e-010 v Velocity[Y] -0.44564 1.1694 0.016512 0.016512 v Velocity[Z] -6.7905e-014 7.3644e-014 -1.6076e-016 -1.6076e-016 v ǁVelocityǁ 5.5224e-006 1.1702 0.035715 0.035715 v Pressure -1.0116 0.99994 5.7732e-016 1.1926e-015 v TempK 292.73 298.48 293.23 293.23 v Density 1 1 1 1 v CourantNb 8.1492e-005 8 0.12294 0.12294 v FourierNb 0.080866 0.16173 0.15969 0.15969 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25935 0.34523 0.34519 0.34519 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.74 303.15 293.28 293.27 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12138 8.154 0.28263 0.28263 INSTANT 0.140000000E+01 TIME STEP NUMBER 14 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.39918E-04 0.45040E-01 Friction velocity uk : 0.39918E-04 0.45040E-01 Dimensionless distance yplus : 0.13633E-01 0.15382E+02 Friction thermal sca. tstar : -0.19162E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.96794E-02 0.10921E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10719E-03 55 0.25628E+00 0.25150E-02 0.50735E+00 c Velocity[X] 0.21303E-03 c Velocity[Y] 0.23019E-02 c Velocity[Z] 0.16915E-29 c Pressure 0.31092E-03 12 0.41502E-07 0.18461E+00 0.28723E-02 c TempK 0.97178E+02 26 0.18273E-03 0.74803E-02 0.47863E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.31473 0.31461 4.3651e-010 4.3651e-010 v Velocity[Y] -0.5472 1.3185 0.017129 0.017129 v Velocity[Z] -6.9705e-014 7.4742e-014 -1.6492e-016 -1.6492e-016 v ǁVelocityǁ 1.4898e-005 1.3186 0.037505 0.037505 v Pressure -1.0163 1.0006 -1.9096e-015 -1.2902e-015 v TempK 292.71 298.62 293.24 293.24 v Density 1 1 1 1 v CourantNb 0.00021397 8 0.17763 0.17763 v FourierNb 0.088953 0.17791 0.17566 0.17566 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27301 0.37975 0.37969 0.37969 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.73 303.15 293.29 293.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13392 8.1596 0.35329 0.35329 INSTANT 0.150000000E+01 TIME STEP NUMBER 15 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13582E-03 0.37553E-01 Friction velocity uk : 0.13582E-03 0.37553E-01 Dimensionless distance yplus : 0.46388E-01 0.12826E+02 Friction thermal sca. tstar : -0.42338E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.32935E-01 0.91060E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.13778E-03 73 0.27214E+00 0.36452E-02 0.59867E+00 c Velocity[X] 0.29807E-03 c Velocity[Y] 0.33472E-02 c Velocity[Z] 0.26681E-29 c Pressure 0.38070E-03 12 0.53885E-07 0.21360E+00 0.35467E-02 c TempK 0.88465E+02 28 0.28913E-03 0.72147E-02 0.44819E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.35136 0.35117 2.1137e-009 2.1137e-009 v Velocity[Y] -0.52729 1.3397 0.017361 0.017361 v Velocity[Z] -7.1406e-014 7.5206e-014 -1.6806e-016 -1.6806e-016 v ǁVelocityǁ 3.2388e-005 1.3404 0.038356 0.038356 v Pressure -1.0211 1.0003 -1.4833e-015 -9.4326e-016 v TempK 292.25 298.93 293.24 293.24 v Density 1 1 1 1 v CourantNb 0.0006725 8 0.2646 0.2646 v FourierNb 0.090701 0.1957 0.19313 0.19313 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.22363 0.41772 0.41743 0.41743 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.71 303.15 293.3 293.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14912 8.1835 0.45772 0.45772 INSTANT 0.160000000E+01 TIME STEP NUMBER 16 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.19792E-03 0.42486E-01 Friction velocity uk : 0.19792E-03 0.42486E-01 Dimensionless distance yplus : 0.67594E-01 0.14510E+02 Friction thermal sca. tstar : -0.25194E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.47991E-01 0.10302E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.17622E-03 67 0.33949E+00 0.65023E-02 0.78953E+00 c Velocity[X] 0.42801E-03 c Velocity[Y] 0.60742E-02 c Velocity[Z] 0.39080E-29 c Pressure 0.54927E-03 12 0.80320E-07 0.29222E+00 0.45249E-02 c TempK 0.80552E+02 32 0.41369E-03 0.71699E-02 0.42599E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.32366 0.27514 -2.3005e-009 -2.3005e-009 v Velocity[Y] -0.65006 1.4506 0.016464 0.016464 v Velocity[Z] -7.0905e-014 7.4759e-014 -1.7005e-016 -1.7005e-016 v ǁVelocityǁ 3.6103e-005 1.4509 0.03741 0.03741 v Pressure -1.0156 1.0021 -3.2863e-016 2.8189e-016 v TempK 291.78 299.23 293.25 293.25 v Density 1 1 1 1 v CourantNb 0.0016308 8 0.41629 0.41629 v FourierNb 0.075615 0.21527 0.21236 0.21236 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.18337 0.4595 0.459 0.459 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.25 303.15 293.3 293.29 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.17872 8.2143 0.62866 0.62866 INSTANT 0.170000000E+01 TIME STEP NUMBER 17 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.68584E-03 0.36221E-01 Friction velocity uk : 0.68584E-03 0.36221E-01 Dimensionless distance yplus : 0.23424E+00 0.12370E+02 Friction thermal sca. tstar : -0.24334E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.16630E+00 0.87828E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29180E-03 95 0.41772E+00 0.12013E-01 0.13019E+01 c Velocity[X] 0.53924E-03 c Velocity[Y] 0.11473E-01 c Velocity[Z] 0.70034E-29 c Pressure 0.70633E-03 19 0.79127E-08 0.38211E+00 0.72786E-02 c TempK 0.73960E+02 37 0.45398E-03 0.64125E-02 0.38487E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.29542 0.3131 -1.0791e-008 -1.0791e-008 v Velocity[Y] -0.63786 1.5202 0.013569 0.013569 v Velocity[Z] -6.7083e-014 8.6335e-014 -1.6205e-016 -1.6205e-016 v ǁVelocityǁ 1.6844e-005 1.522 0.035143 0.035143 v Pressure -1.0231 1.0037 4.1744e-016 1.03e-015 v TempK 291.72 299.51 293.26 293.26 v Density 1 1 1 1 v CourantNb 0.001783 8 0.66604 0.66604 v FourierNb 0.069936 0.23679 0.23276 0.23276 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.18099 0.50545 0.50289 0.50289 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.78 303.15 293.31 293.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.19253 8.2351 0.89879 0.89879 INSTANT 0.180000000E+01 TIME STEP NUMBER 18 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.45220E-03 0.41407E-01 Friction velocity uk : 0.45220E-03 0.41407E-01 Dimensionless distance yplus : 0.15444E+00 0.14142E+02 Friction thermal sca. tstar : -0.34302E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.10965E+00 0.10040E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30380E-03 99 0.42242E+00 0.10897E-01 0.15065E+01 c Velocity[X] 0.50962E-03 c Velocity[Y] 0.10388E-01 c Velocity[Z] 0.10308E-28 c Pressure 0.61191E-03 13 0.89265E-07 0.34965E+00 0.49075E-02 c TempK 0.68117E+02 37 0.42568E-03 0.70182E-02 0.38511E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.25281 0.3041 -1.4933e-008 -1.4933e-008 v Velocity[Y] -0.54887 1.1562 0.010818 0.010818 v Velocity[Z] -6.5388e-014 6.8663e-014 -1.5423e-016 -1.5423e-016 v ǁVelocityǁ 1.0328e-005 1.1568 0.033089 0.033089 v Pressure -1.0232 1.0056 -1.1191e-015 -4.9873e-016 v TempK 291.68 300.05 293.27 293.27 v Density 1 1 1 1 v CourantNb 0.0016997 8 0.91331 0.91331 v FourierNb 0.069751 0.26047 0.25484 0.25484 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.19802 0.55599 0.55035 0.55035 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.72 303.15 293.32 293.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.20932 8.26 1.1681 1.1681 INSTANT 0.190000000E+01 TIME STEP NUMBER 19 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.62256E-03 0.36208E-01 Friction velocity uk : 0.62256E-03 0.36208E-01 Dimensionless distance yplus : 0.21262E+00 0.12366E+02 Friction thermal sca. tstar : -0.22276E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.15096E+00 0.87797E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.20942E-03 96 0.37693E+00 0.60473E-02 0.12121E+01 c Velocity[X] 0.41095E-03 c Velocity[Y] 0.56363E-02 c Velocity[Z] 0.82590E-29 c Pressure 0.49186E-03 12 0.51601E-07 0.27664E+00 0.33149E-02 c TempK 0.62291E+02 38 0.38430E-03 0.67057E-02 0.36010E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22109 0.22131 -2.4607e-008 -2.4607e-008 v Velocity[Y] -0.49734 0.99614 0.0098185 0.0098185 v Velocity[Z] -6.5582e-014 7.0128e-014 -1.534e-016 -1.534e-016 v ǁVelocityǁ 7.1521e-006 0.99622 0.031418 0.031418 v Pressure -1.0215 1.0028 -1.1191e-015 -5.3126e-016 v TempK 291.67 300.8 293.28 293.28 v Density 1 1 1 1 v CourantNb 0.00070816 8 1.0035 1.0035 v FourierNb 0.068296 0.28652 0.27962 0.27962 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.19438 0.61159 0.60383 0.60383 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.68 303.15 293.33 293.32 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.2277 8.2851 1.2831 1.2831 INSTANT 0.200000000E+01 TIME STEP NUMBER 20 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.24827E-03 0.41434E-01 Friction velocity uk : 0.24827E-03 0.41434E-01 Dimensionless distance yplus : 0.84793E-01 0.14151E+02 Friction thermal sca. tstar : -0.54122E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.60202E-01 0.10047E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.15029E-03 83 0.35042E+00 0.40066E-02 0.96539E+00 c Velocity[X] 0.34522E-03 c Velocity[Y] 0.36614E-02 c Velocity[Z] 0.62739E-29 c Pressure 0.43505E-03 12 0.50506E-07 0.23402E+00 0.27394E-02 c TempK 0.56923E+02 38 0.34506E-03 0.64758E-02 0.33904E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16339 0.16619 -7.2672e-009 -7.2672e-009 v Velocity[Y] -0.43316 0.85816 0.0099462 0.0099462 v Velocity[Z] -6.5673e-014 6.9964e-014 -1.4169e-016 -1.4169e-016 v ǁVelocityǁ 4.4465e-005 0.85834 0.030981 0.030981 v Pressure -1.0136 1.0022 -1.7408e-015 -1.1059e-015 v TempK 291.65 301.29 293.29 293.29 v Density 1 1 1 1 v CourantNb 0.00049274 8 1.0645 1.0645 v FourierNb 0.075126 0.31517 0.30683 0.30683 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.21381 0.67275 0.66256 0.66256 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.67 303.15 293.34 293.33 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.24758 8.315 1.3713 1.3713 INSTANT 0.210000000E+01 TIME STEP NUMBER 21 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26213E-03 0.36674E-01 Friction velocity uk : 0.26213E-03 0.36674E-01 Dimensionless distance yplus : 0.89525E-01 0.12525E+02 Friction thermal sca. tstar : -0.26785E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.63561E-01 0.88928E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.12127E-03 81 0.31471E+00 0.32602E-02 0.82675E+00 c Velocity[X] 0.33967E-03 c Velocity[Y] 0.29205E-02 c Velocity[Z] 0.56359E-29 c Pressure 0.39863E-03 12 0.51450E-07 0.20260E+00 0.19753E-02 c TempK 0.52149E+02 44 0.41015E-03 0.65022E-02 0.32208E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15401 0.16217 -4.311e-009 -4.311e-009 v Velocity[Y] -0.42039 0.81854 0.010729 0.010729 v Velocity[Z] -6.56e-014 7.3103e-014 -1.4053e-016 -1.4053e-016 v ǁVelocityǁ 5.2552e-005 0.8218 0.032111 0.032111 v Pressure -1.01 1.0018 -6.1284e-016 -2.1684e-017 v TempK 291.44 301.47 293.3 293.3 v Density 1 1 1 1 v CourantNb 0.0036849 8 1.19 1.19 v FourierNb 0.082638 0.34669 0.33636 0.33636 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2352 0.74002 0.72632 0.72632 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.65 303.15 293.35 293.34 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.26973 8.3451 1.5264 1.5264 INSTANT 0.220000000E+01 TIME STEP NUMBER 22 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10341E-03 0.41630E-01 Friction velocity uk : 0.10341E-03 0.41630E-01 Dimensionless distance yplus : 0.35316E-01 0.14218E+02 Friction thermal sca. tstar : -0.11404E+03 0.00000E+00 Rough dim-less th. sca. tplus : 0.25074E-01 0.10094E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10931E-03 85 0.32122E+00 0.31862E-02 0.78128E+00 c Velocity[X] 0.39000E-03 c Velocity[Y] 0.27962E-02 c Velocity[Z] 0.52734E-29 c Pressure 0.38377E-03 12 0.52136E-07 0.18356E+00 0.15173E-02 c TempK 0.47884E+02 49 0.50256E-03 0.79993E-02 0.34362E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21274 0.20731 7.6318e-008 7.6318e-008 v Velocity[Y] -0.37666 0.83155 0.011605 0.011605 v Velocity[Z] -6.5437e-014 7.0761e-014 -1.3453e-016 -1.3453e-016 v ǁVelocityǁ 4.2459e-005 0.83223 0.034422 0.034422 v Pressure -1.0083 1.0023 -2.2204e-016 4.0115e-016 v TempK 291.39 301.37 293.31 293.31 v Density 1 1 1 1 v CourantNb 0.0060077 8 1.3968 1.3968 v FourierNb 0.090902 0.38136 0.36857 0.36857 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25871 0.81403 0.79585 0.79585 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.44 303.15 293.36 293.35 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.29424 8.3798 1.7654 1.7654 INSTANT 0.230000000E+01 TIME STEP NUMBER 23 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10700E-03 0.39027E-01 Friction velocity uk : 0.10700E-03 0.39027E-01 Dimensionless distance yplus : 0.36543E-01 0.13329E+02 Friction thermal sca. tstar : -0.68631E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.25945E-01 0.94633E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10435E-03 90 0.31059E+00 0.33368E-02 0.78889E+00 c Velocity[X] 0.43920E-03 c Velocity[Y] 0.28976E-02 c Velocity[Z] 0.56039E-29 c Pressure 0.36747E-03 12 0.52770E-07 0.16773E+00 0.13244E-02 c TempK 0.44201E+02 52 0.79536E-03 0.11597E-01 0.41432E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24393 0.21756 2.0468e-007 2.0468e-007 v Velocity[Y] -0.36655 0.86261 0.012139 0.012139 v Velocity[Z] -6.4818e-014 7.0666e-014 -1.3289e-016 -1.3289e-016 v ǁVelocityǁ 5.5015e-005 0.86464 0.036067 0.036067 v Pressure -1.0083 1.0036 -6.2172e-017 5.7463e-016 v TempK 291.74 301.55 293.32 293.32 v Density 1 1 1 1 v CourantNb 0.0063612 8 1.7042 1.7042 v FourierNb 0.099992 0.41949 0.40285 0.40285 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28459 0.89543 0.86971 0.86971 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.39 303.15 293.37 293.36 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.32098 8.4193 2.107 2.107 INSTANT 0.240000000E+01 TIME STEP NUMBER 24 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.27875E-03 0.43810E-01 Friction velocity uk : 0.27875E-03 0.43810E-01 Dimensionless distance yplus : 0.95201E-01 0.14963E+02 Friction thermal sca. tstar : -0.37449E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.67591E-01 0.10623E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10244E-03 93 0.32003E+00 0.34344E-02 0.78654E+00 c Velocity[X] 0.49898E-03 c Velocity[Y] 0.29354E-02 c Velocity[Z] 0.65044E-29 c Pressure 0.35758E-03 11 0.52070E-07 0.15781E+00 0.13384E-02 c TempK 0.41377E+02 65 0.10795E-02 0.16010E-01 0.49033E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.3036 0.24558 -4.0586e-007 -4.0586e-007 v Velocity[Y] -0.32685 0.9422 0.012386 0.012386 v Velocity[Z] -6.5538e-014 6.9465e-014 -1.249e-016 -1.249e-016 v ǁVelocityǁ 5.8781e-005 0.9434 0.037944 0.037944 v Pressure -1.008 1.0038 -2.6645e-016 3.9031e-016 v TempK 292.21 301.6 293.33 293.33 v Density 1 1 1 1 v CourantNb 0.0076576 8 1.9324 1.9324 v FourierNb 0.10999 0.46144 0.43868 0.43868 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31039 0.98497 0.94685 0.94685 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.74 303.15 293.38 293.37 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.35374 8.4605 2.3711 2.3711 INSTANT 0.250000000E+01 TIME STEP NUMBER 25 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.24500E-03 0.42864E-01 Friction velocity uk : 0.24500E-03 0.42864E-01 Dimensionless distance yplus : 0.83675E-01 0.14640E+02 Friction thermal sca. tstar : -0.31474E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.59408E-01 0.10394E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10459E-03 95 0.31610E+00 0.37467E-02 0.82790E+00 c Velocity[X] 0.56014E-03 c Velocity[Y] 0.31866E-02 c Velocity[Z] 0.60229E-29 c Pressure 0.35966E-03 12 0.54579E-07 0.15416E+00 0.14657E-02 c TempK 0.39055E+02 62 0.10799E-02 0.14359E-01 0.43510E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24763 0.24168 -9.0013e-007 -9.0013e-007 v Velocity[Y] -0.32049 0.91237 0.012609 0.012609 v Velocity[Z] -6.5728e-014 7.1663e-014 -1.3211e-016 -1.3211e-016 v ǁVelocityǁ 5.7773e-005 0.91339 0.038981 0.038981 v Pressure -1.0077 1.0043 -1.3323e-016 6.0715e-016 v TempK 292.22 301.75 293.35 293.35 v Density 1 1 1 1 v CourantNb 0.0086542 8 2.2481 2.2481 v FourierNb 0.11595 0.50758 0.4766 0.4766 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29832 1.0835 1.0284 1.0284 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.21 303.15 293.39 293.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.38934 8.5064 2.7247 2.7247 INSTANT 0.260000000E+01 TIME STEP NUMBER 26 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.33855E-03 0.47578E-01 Friction velocity uk : 0.33855E-03 0.47578E-01 Dimensionless distance yplus : 0.11562E+00 0.16249E+02 Friction thermal sca. tstar : -0.27207E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.82091E-01 0.11537E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10447E-03 97 0.31312E+00 0.40124E-02 0.85541E+00 c Velocity[X] 0.62083E-03 c Velocity[Y] 0.33916E-02 c Velocity[Z] 0.55152E-29 c Pressure 0.35953E-03 12 0.55352E-07 0.15157E+00 0.15441E-02 c TempK 0.36953E+02 62 0.96934E-03 0.25140E-01 0.53731E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.25425 0.25924 -2.7438e-006 -2.7438e-006 v Velocity[Y] -0.33295 1.0353 0.012566 0.012566 v Velocity[Z] -6.6111e-014 6.9352e-014 -1.2235e-016 -1.2235e-016 v ǁVelocityǁ 7.9788e-005 1.0378 0.040191 0.040191 v Pressure -1.0073 1.0044 -1.199e-015 -6.6136e-016 v TempK 291.81 301.79 293.36 293.36 v Density 1 1 1 1 v CourantNb 0.0083833 8 2.4604 2.4604 v FourierNb 0.12167 0.55834 0.51764 0.51764 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30632 1.1918 1.1167 1.1167 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.22 303.15 293.4 293.39 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.42714 8.5562 2.978 2.978 INSTANT 0.270000000E+01 TIME STEP NUMBER 27 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.36515E-03 0.47123E-01 Friction velocity uk : 0.36515E-03 0.47123E-01 Dimensionless distance yplus : 0.12471E+00 0.16094E+02 Friction thermal sca. tstar : -0.23535E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.88543E-01 0.11426E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10866E-03 98 0.31254E+00 0.43431E-02 0.90953E+00 c Velocity[X] 0.67676E-03 c Velocity[Y] 0.36664E-02 c Velocity[Z] 0.60553E-29 c Pressure 0.36139E-03 11 0.55906E-07 0.14862E+00 0.15584E-02 c TempK 0.35352E+02 58 0.95626E-03 0.16168E-01 0.42366E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24487 0.25255 -4.9276e-006 -4.9276e-006 v Velocity[Y] -0.39771 1.0086 0.012414 0.012414 v Velocity[Z] -6.8444e-014 6.9425e-014 -1.3649e-016 -1.3649e-016 v ǁVelocityǁ 5.8857e-005 1.0121 0.040997 0.040997 v Pressure -1.0069 1.0062 -4.7962e-016 1.301e-016 v TempK 292.07 301.98 293.38 293.38 v Density 1 1 1 1 v CourantNb 0.014552 8 2.7589 2.7589 v FourierNb 0.12568 0.61418 0.56221 0.56221 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26827 1.311 1.2124 1.2124 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.81 303.15 293.42 293.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.47519 8.6126 3.3211 3.3211 INSTANT 0.280000000E+01 TIME STEP NUMBER 28 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.44848E-03 0.52924E-01 Friction velocity uk : 0.44848E-03 0.52924E-01 Dimensionless distance yplus : 0.15317E+00 0.18075E+02 Friction thermal sca. tstar : -0.27505E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.10875E+00 0.12833E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10998E-03 101 0.31373E+00 0.43835E-02 0.91216E+00 c Velocity[X] 0.70516E-03 c Velocity[Y] 0.36784E-02 c Velocity[Z] 0.59384E-29 c Pressure 0.37940E-03 12 0.59133E-07 0.15139E+00 0.17205E-02 c TempK 0.34033E+02 66 0.90399E-03 0.20456E-01 0.45851E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21551 0.25106 1.1014e-006 1.1014e-006 v Velocity[Y] -0.39803 0.95464 0.012302 0.012302 v Velocity[Z] -6.8941e-014 6.6906e-014 -1.28e-016 -1.28e-016 v ǁVelocityǁ 0.00010542 0.95499 0.042301 0.042301 v Pressure -1.0081 1.0059 8.1712e-016 1.442e-015 v TempK 291.66 302.05 293.4 293.4 v Density 1 1 1 1 v CourantNb 0.0099686 8 3.0131 3.0131 v FourierNb 0.10516 0.67559 0.60934 0.60934 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27088 1.4421 1.3137 1.3137 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.07 303.15 293.43 293.42 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.51666 8.6752 3.6224 3.6224 INSTANT 0.290000000E+01 TIME STEP NUMBER 29 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.34671E-03 0.52869E-01 Friction velocity uk : 0.34671E-03 0.52869E-01 Dimensionless distance yplus : 0.11841E+00 0.18057E+02 Friction thermal sca. tstar : -0.21555E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.84070E-01 0.12820E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10915E-03 99 0.33168E+00 0.40462E-02 0.88375E+00 c Velocity[X] 0.70400E-03 c Velocity[Y] 0.33422E-02 c Velocity[Z] 0.55689E-29 c Pressure 0.37977E-03 12 0.59306E-07 0.14705E+00 0.16359E-02 c TempK 0.33012E+02 73 0.86777E-03 0.17168E-01 0.44514E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24977 0.26107 1.7311e-005 1.7311e-005 v Velocity[Y] -0.40891 1.1111 0.012331 0.012331 v Velocity[Z] -6.8197e-014 6.9987e-014 -1.3586e-016 -1.3586e-016 v ǁVelocityǁ 0.00010679 1.1111 0.042759 0.042759 v Pressure -1.0079 1.0076 -1.9007e-015 -1.236e-015 v TempK 290.33 302.17 293.42 293.42 v Density 1 1 1 1 v CourantNb 0.027443 8 3.3667 3.3667 v FourierNb 0.10773 0.74315 0.65848 0.65848 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28462 1.5863 1.4194 1.4194 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.66 303.15 293.45 293.44 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.58481 8.743 4.0251 4.0251 INSTANT 0.300000000E+01 TIME STEP NUMBER 30 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10440E-03 0.57038E-01 Friction velocity uk : 0.10440E-03 0.57038E-01 Dimensionless distance yplus : 0.35656E-01 0.19480E+02 Friction thermal sca. tstar : -0.67586E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.25315E-01 0.13831E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10869E-03 102 0.32532E+00 0.42959E-02 0.89914E+00 c Velocity[X] 0.72716E-03 c Velocity[Y] 0.35687E-02 c Velocity[Z] 0.45425E-29 c Pressure 0.38045E-03 12 0.56694E-07 0.14069E+00 0.17856E-02 c TempK 0.32070E+02 73 0.11134E-02 0.19750E-01 0.46128E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23094 0.27197 1.4144e-005 1.4144e-005 v Velocity[Y] -0.30601 1.339 0.012372 0.012372 v Velocity[Z] -6.7947e-014 7.0835e-014 -1.2086e-016 -1.2086e-016 v ǁVelocityǁ 0.00024753 1.3395 0.044156 0.044156 v Pressure -1.0084 1.0054 -5.862e-016 4.3368e-017 v TempK 289.39 302.27 293.44 293.44 v Density 1 1 1 1 v CourantNb 0.030335 8 3.5973 3.5973 v FourierNb 0.10152 0.81747 0.7121 0.7121 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.23169 1.7449 1.5345 1.5345 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.33 303.15 293.47 293.46 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.5372 8.817 4.3094 4.3094 INSTANT 0.310000000E+01 TIME STEP NUMBER 31 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.45014E-03 0.62615E-01 Friction velocity uk : 0.45014E-03 0.62615E-01 Dimensionless distance yplus : 0.15373E+00 0.21385E+02 Friction thermal sca. tstar : -0.80800E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.10915E+00 0.15183E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10365E-03 102 0.31623E+00 0.44313E-02 0.93738E+00 c Velocity[X] 0.73073E-03 c Velocity[Y] 0.37006E-02 c Velocity[Z] 0.53213E-29 c Pressure 0.37627E-03 12 0.57027E-07 0.13515E+00 0.17948E-02 c TempK 0.31547E+02 75 0.18143E-02 0.17074E-01 0.40903E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24772 0.34789 1.3967e-005 1.3967e-005 v Velocity[Y] -0.28873 1.0562 0.012056 0.012056 v Velocity[Z] -6.741e-014 7.2385e-014 -1.4696e-016 -1.4696e-016 v ǁVelocityǁ 3.3645e-005 1.0563 0.044595 0.044595 v Pressure -1.0083 1.0068 -3.4639e-016 2.3852e-016 v TempK 289.06 302.41 293.47 293.47 v Density 1 1 1 1 v CourantNb 0.062031 8 3.9626 3.9626 v FourierNb 0.096465 0.89922 0.76716 0.76716 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.24584 1.9194 1.6528 1.6528 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 289.39 303.15 293.5 293.49 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.50353 8.8989 4.7298 4.7298 INSTANT 0.320000000E+01 TIME STEP NUMBER 32 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.17602E-03 0.46898E-01 Friction velocity uk : 0.17602E-03 0.46898E-01 Dimensionless distance yplus : 0.60117E-01 0.16017E+02 Friction thermal sca. tstar : -0.18506E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.42682E-01 0.11372E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10421E-03 103 0.29939E+00 0.43530E-02 0.92502E+00 c Velocity[X] 0.73641E-03 c Velocity[Y] 0.36166E-02 c Velocity[Z] 0.53236E-29 c Pressure 0.36214E-03 12 0.54102E-07 0.12375E+00 0.16749E-02 c TempK 0.31096E+02 81 0.12141E-02 0.17435E-01 0.45140E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23526 0.2965 -3.7902e-006 -3.7902e-006 v Velocity[Y] -0.32997 0.88105 0.011902 0.011902 v Velocity[Z] -6.7358e-014 6.9044e-014 -1.3602e-016 -1.3602e-016 v ǁVelocityǁ 0.00027797 0.8834 0.046438 0.046438 v Pressure -1.0077 1.0054 -4.7962e-016 7.5894e-017 v TempK 289.12 302.55 293.5 293.5 v Density 1 1 1 1 v CourantNb 0.010837 8 4.2803 4.2803 v FourierNb 0.093359 0.98914 0.8248 0.8248 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.19928 2.1114 1.7766 1.7766 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 289.06 303.15 293.52 293.51 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.58363 8.9888 5.1051 5.1051 INSTANT 0.330000000E+01 TIME STEP NUMBER 33 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.75525E-03 0.47133E-01 Friction velocity uk : 0.75525E-03 0.47133E-01 Dimensionless distance yplus : 0.25794E+00 0.16097E+02 Friction thermal sca. tstar : -0.84173E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.18313E+00 0.11429E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.99624E-04 108 0.30760E+00 0.41210E-02 0.91171E+00 c Velocity[X] 0.68660E-03 c Velocity[Y] 0.34344E-02 c Velocity[Z] 0.53859E-29 c Pressure 0.35158E-03 11 0.54533E-07 0.11292E+00 0.16973E-02 c TempK 0.30801E+02 85 0.10541E-02 0.20115E-01 0.42357E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.252 0.23806 1.8032e-005 1.8032e-005 v Velocity[Y] -0.31561 0.89723 0.011965 0.011965 v Velocity[Z] -6.6973e-014 6.5558e-014 -1.4246e-016 -1.4246e-016 v ǁVelocityǁ 0.00016177 0.90791 0.048142 0.048142 v Pressure -1.0074 1.0088 4.4409e-017 7.2642e-016 v TempK 289.33 302.77 293.53 293.53 v Density 1 1 1 1 v CourantNb 0.06982 8 4.7118 4.7118 v FourierNb 0.10269 1.0881 0.87776 0.87776 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.21921 2.3225 1.8907 1.8907 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 289.12 303.15 293.55 293.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60578 9.0875 5.5896 5.5896 INSTANT 0.340000000E+01 TIME STEP NUMBER 34 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11668E-03 0.46462E-01 Friction velocity uk : 0.11668E-03 0.46462E-01 Dimensionless distance yplus : 0.39851E-01 0.15868E+02 Friction thermal sca. tstar : -0.65761E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.28294E-01 0.11266E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10178E-03 107 0.30279E+00 0.37628E-02 0.84434E+00 c Velocity[X] 0.65595E-03 c Velocity[Y] 0.31069E-02 c Velocity[Z] 0.52614E-29 c Pressure 0.35810E-03 11 0.60702E-07 0.10831E+00 0.18444E-02 c TempK 0.30647E+02 88 0.10024E-02 0.18523E-01 0.43520E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21901 0.26924 4.1261e-006 4.1261e-006 v Velocity[Y] -0.32611 1.0619 0.012023 0.012023 v Velocity[Z] -6.7297e-014 6.2975e-014 -1.2975e-016 -1.2975e-016 v ǁVelocityǁ 0.00026949 1.0621 0.049555 0.049555 v Pressure -1.0071 1.0056 -1.2346e-015 -6.2884e-016 v TempK 289.68 303.15 293.56 293.56 v Density 1 1 1 1 v CourantNb 0.043776 8 5.1853 5.1853 v FourierNb 0.11296 1.1969 0.92939 0.92939 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.24113 2.5548 2.002 2.002 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 289.33 303.15 293.58 293.57 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.68643 9.1965 6.1147 6.1147 INSTANT 0.350000000E+01 TIME STEP NUMBER 35 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.17297E-03 0.48909E-01 Friction velocity uk : 0.17297E-03 0.48909E-01 Dimensionless distance yplus : 0.59074E-01 0.16704E+02 Friction thermal sca. tstar : -0.34827E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.41941E-01 0.11859E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97222E-04 108 0.30723E+00 0.37535E-02 0.81998E+00 c Velocity[X] 0.65424E-03 c Velocity[Y] 0.30992E-02 c Velocity[Z] 0.53871E-29 c Pressure 0.35877E-03 11 0.53206E-07 0.10140E+00 0.16051E-02 c TempK 0.30374E+02 90 0.10553E-02 0.17129E-01 0.37214E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20438 0.29945 1.531e-005 1.531e-005 v Velocity[Y] -0.30146 1.0695 0.01208 0.01208 v Velocity[Z] -6.8017e-014 6.2763e-014 -1.4591e-016 -1.4591e-016 v ǁVelocityǁ 0.00019864 1.0707 0.051315 0.051315 v Pressure -1.0061 1.0071 -7.1054e-017 4.7705e-016 v TempK 290.07 303.77 293.6 293.6 v Density 1 1 1 1 v CourantNb 0.11993 8 5.5588 5.5588 v FourierNb 0.12426 1.3165 0.97958 0.97958 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26524 2.8102 2.1101 2.1101 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 289.68 303.15 293.61 293.6 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81317 9.3157 6.5384 6.5384 INSTANT 0.360000000E+01 TIME STEP NUMBER 36 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.19957E-03 0.47313E-01 Friction velocity uk : 0.19957E-03 0.47313E-01 Dimensionless distance yplus : 0.68160E-01 0.16159E+02 Friction thermal sca. tstar : -0.10278E+02 0.62030E+00 Rough dim-less th. sca. tplus : 0.48392E-01 0.11472E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94203E-04 113 0.30739E+00 0.39778E-02 0.86317E+00 c Velocity[X] 0.67535E-03 c Velocity[Y] 0.33024E-02 c Velocity[Z] 0.56716E-29 c Pressure 0.35751E-03 11 0.49034E-07 0.94767E-01 0.15275E-02 c TempK 0.30317E+02 91 0.10084E-02 0.17505E-01 0.38897E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21387 0.25379 -7.1386e-006 -7.1386e-006 v Velocity[Y] -0.26853 0.88155 0.011851 0.011851 v Velocity[Z] -6.8757e-014 6.151e-014 -1.4074e-016 -1.4074e-016 v ǁVelocityǁ 8.6452e-005 0.88277 0.052165 0.052165 v Pressure -1.0052 1.0061 -4.7073e-016 7.5894e-017 v TempK 290.51 304.05 293.64 293.64 v Density 1 1 1 1 v CourantNb 0.11484 8 6.0157 6.0157 v FourierNb 0.12428 1.4482 1.0179 1.0179 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26529 3.0913 2.1932 2.1932 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.07 303.77 293.65 293.64 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.82609 9.4479 7.0336 7.0336 INSTANT 0.370000000E+01 TIME STEP NUMBER 37 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.42597E-03 0.48917E-01 Friction velocity uk : 0.42597E-03 0.48917E-01 Dimensionless distance yplus : 0.14548E+00 0.16707E+02 Friction thermal sca. tstar : -0.10224E+02 0.88464E+00 Rough dim-less th. sca. tplus : 0.10329E+00 0.11861E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87386E-04 117 0.30781E+00 0.38580E-02 0.84393E+00 c Velocity[X] 0.69222E-03 c Velocity[Y] 0.31658E-02 c Velocity[Z] 0.46125E-29 c Pressure 0.36313E-03 11 0.52472E-07 0.88899E-01 0.16378E-02 c TempK 0.30171E+02 89 0.10493E-02 0.16816E-01 0.35861E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.224 0.2234 7.175e-006 7.175e-006 v Velocity[Y] -0.27115 0.9415 0.011779 0.011779 v Velocity[Z] -6.6058e-014 6.1341e-014 -1.4669e-016 -1.4669e-016 v ǁVelocityǁ 0.0005443 0.94499 0.053658 0.053658 v Pressure -1.0053 1.0087 7.0166e-016 1.3119e-015 v TempK 290.92 303.55 293.68 293.68 v Density 1 1 1 1 v CourantNb 0.046613 8 6.2843 6.2843 v FourierNb 0.13671 1.593 1.0414 1.0414 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29182 3.4004 2.2446 2.2446 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.51 304.05 293.69 293.68 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73017 9.592 7.3257 7.3257 INSTANT 0.380000000E+01 TIME STEP NUMBER 38 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12351E-02 0.45403E-01 Friction velocity uk : 0.12351E-02 0.45403E-01 Dimensionless distance yplus : 0.42182E+00 0.15507E+02 Friction thermal sca. tstar : -0.48033E+01 0.47353E+00 Rough dim-less th. sca. tplus : 0.29948E+00 0.11009E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89048E-04 117 0.30155E+00 0.39075E-02 0.83900E+00 c Velocity[X] 0.66377E-03 c Velocity[Y] 0.32438E-02 c Velocity[Z] 0.52925E-29 c Pressure 0.36250E-03 11 0.40314E-07 0.81972E-01 0.15277E-02 c TempK 0.30390E+02 89 0.10852E-02 0.19977E-01 0.42259E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22361 0.21298 -2.1871e-005 -2.1871e-005 v Velocity[Y] -0.26973 0.90857 0.012042 0.012042 v Velocity[Z] -6.517e-014 6.0222e-014 -1.2896e-016 -1.2896e-016 v ǁVelocityǁ 0.00022028 0.91583 0.05501 0.05501 v Pressure -1.0056 1.0055 -3.7303e-016 2.06e-016 v TempK 291.2 303.49 293.71 293.71 v Density 1 1 1 1 v CourantNb 0.25011 8 6.5402 6.5402 v FourierNb 0.11245 1.7523 1.0563 1.0563 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.24004 3.7404 2.2771 2.2771 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.92 303.55 293.73 293.72 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.52933 9.7521 7.5965 7.5965 INSTANT 0.390000000E+01 TIME STEP NUMBER 39 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10628E-02 0.47992E-01 Friction velocity uk : 0.10628E-02 0.47992E-01 Dimensionless distance yplus : 0.36299E+00 0.16391E+02 Friction thermal sca. tstar : -0.21380E+02 0.25393E+00 Rough dim-less th. sca. tplus : 0.25772E+00 0.11637E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87819E-04 118 0.30863E+00 0.38178E-02 0.79684E+00 c Velocity[X] 0.67854E-03 c Velocity[Y] 0.31392E-02 c Velocity[Z] 0.59179E-29 c Pressure 0.35301E-03 12 0.38165E-07 0.72918E-01 0.14138E-02 c TempK 0.30577E+02 88 0.10693E-02 0.20603E-01 0.43113E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23564 0.23792 -7.8382e-006 -7.8382e-006 v Velocity[Y] -0.26678 1.0955 0.012014 0.012014 v Velocity[Z] -6.7375e-014 6.0433e-014 -1.2161e-016 -1.2161e-016 v ǁVelocityǁ 0.00056973 1.0967 0.056954 0.056954 v Pressure -1.0058 1.007 -5.3291e-017 5.5294e-016 v TempK 291.37 303.26 293.74 293.74 v Density 1 1 1 1 v CourantNb 0.12322 8 6.7642 6.7642 v FourierNb 0.10365 1.9276 1.0673 1.0673 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.22126 4.1145 2.2999 2.2999 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.2 303.49 293.76 293.75 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.4347 9.9248 7.8314 7.8314 INSTANT 0.400000000E+01 TIME STEP NUMBER 40 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11503E-02 0.48155E-01 Friction velocity uk : 0.11503E-02 0.48155E-01 Dimensionless distance yplus : 0.39287E+00 0.16446E+02 Friction thermal sca. tstar : -0.48595E+01 0.84091E-01 Rough dim-less th. sca. tplus : 0.27893E+00 0.11677E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87092E-04 121 0.30771E+00 0.39989E-02 0.82616E+00 c Velocity[X] 0.71127E-03 c Velocity[Y] 0.32877E-02 c Velocity[Z] 0.58044E-29 c Pressure 0.36603E-03 11 0.35142E-07 0.68633E-01 0.14593E-02 c TempK 0.31098E+02 91 0.12226E-02 0.26100E-01 0.49378E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18412 0.22858 -1.7799e-005 -1.7799e-005 v Velocity[Y] -0.29254 1.0927 0.012019 0.012019 v Velocity[Z] -6.8591e-014 5.7604e-014 -1.3573e-016 -1.3573e-016 v ǁVelocityǁ 0.00087109 1.1004 0.058381 0.058381 v Pressure -1.0063 1.0073 1.0658e-016 6.6136e-016 v TempK 291.44 303.09 293.76 293.76 v Density 1 1 1 1 v CourantNb 0.21143 8 6.9993 6.9993 v FourierNb 0.11402 2.1203 1.0607 1.0607 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.24338 4.5259 2.286 2.286 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.37 303.26 293.79 293.78 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60602 10.117 8.06 8.06 INSTANT 0.410000000E+01 TIME STEP NUMBER 41 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.60584E-03 0.49376E-01 Friction velocity uk : 0.60584E-03 0.49376E-01 Dimensionless distance yplus : 0.20691E+00 0.16863E+02 Friction thermal sca. tstar : -0.41965E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.14690E+00 0.11973E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.88978E-04 120 0.31326E+00 0.40526E-02 0.83660E+00 c Velocity[X] 0.68412E-03 c Velocity[Y] 0.33685E-02 c Velocity[Z] 0.58960E-29 c Pressure 0.36106E-03 10 0.37335E-07 0.64732E-01 0.15956E-02 c TempK 0.31492E+02 95 0.11717E-02 0.27015E-01 0.50225E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21621 0.24185 9.885e-006 9.885e-006 v Velocity[Y] -0.26078 0.8974 0.011855 0.011855 v Velocity[Z] -6.8792e-014 5.6072e-014 -1.2278e-016 -1.2278e-016 v ǁVelocityǁ 0.00085484 0.89743 0.060031 0.060031 v Pressure -1.0081 1.0097 -1.2523e-015 -6.2884e-016 v TempK 291.42 303.13 293.79 293.79 v Density 1 1 1 1 v CourantNb 0.38922 8 7.1674 7.1674 v FourierNb 0.12292 2.3323 1.0327 1.0327 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26237 4.9785 2.2263 2.2263 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.44 303.15 293.81 293.8 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.76269 10.331 8.2001 8.2001 INSTANT 0.420000000E+01 TIME STEP NUMBER 42 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.43458E-03 0.44287E-01 Friction velocity uk : 0.43458E-03 0.44287E-01 Dimensionless distance yplus : 0.14842E+00 0.15125E+02 Friction thermal sca. tstar : -0.45234E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.10538E+00 0.10739E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91997E-04 117 0.29108E+00 0.41353E-02 0.83851E+00 c Velocity[X] 0.67447E-03 c Velocity[Y] 0.34609E-02 c Velocity[Z] 0.66461E-29 c Pressure 0.35667E-03 11 0.34616E-07 0.62374E-01 0.16804E-02 c TempK 0.32003E+02 96 0.10125E-02 0.31637E-01 0.54332E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.26639 0.22125 -2.262e-005 -2.262e-005 v Velocity[Y] -0.25893 0.95003 0.011886 0.011886 v Velocity[Z] -6.6378e-014 6.1267e-014 -1.3503e-016 -1.3503e-016 v ǁVelocityǁ 0.0011001 0.96222 0.061359 0.061359 v Pressure -1.0134 1.0086 -4.6185e-016 1.8431e-016 v TempK 291.26 303.15 293.8 293.8 v Density 1 1 1 1 v CourantNb 0.36513 8 7.2467 7.2467 v FourierNb 0.097955 2.5656 0.98149 0.98149 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27242 5.4764 2.1166 2.1166 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.42 303.15 293.84 293.83 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73195 10.564 8.2282 8.2282 INSTANT 0.430000000E+01 TIME STEP NUMBER 43 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10504E-02 0.49567E-01 Friction velocity uk : 0.10504E-02 0.49567E-01 Dimensionless distance yplus : 0.35874E+00 0.16929E+02 Friction thermal sca. tstar : -0.48599E+01 0.27489E-02 Rough dim-less th. sca. tplus : 0.25470E+00 0.12019E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.92650E-04 119 0.29736E+00 0.40200E-02 0.82280E+00 c Velocity[X] 0.69545E-03 c Velocity[Y] 0.33246E-02 c Velocity[Z] 0.68409E-29 c Pressure 0.37504E-03 11 0.35289E-07 0.63178E-01 0.17296E-02 c TempK 0.32458E+02 97 0.93287E-03 0.37246E-01 0.57932E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22945 0.22403 -3.62e-006 -3.62e-006 v Velocity[Y] -0.28486 0.85668 0.011889 0.011889 v Velocity[Z] -6.3043e-014 6.1418e-014 -1.236e-016 -1.236e-016 v ǁVelocityǁ 0.00045083 0.85682 0.062348 0.062348 v Pressure -1.0134 1.0084 -1.954e-016 4.2284e-016 v TempK 291.01 303.17 293.83 293.83 v Density 1 1 1 1 v CourantNb 0.11642 8 7.2612 7.2612 v FourierNb 0.089163 2.8221 0.9469 0.9469 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25377 6.024 2.0431 2.0431 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.26 303.15 293.85 293.84 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.31441 10.81 8.2081 8.2081 INSTANT 0.440000000E+01 TIME STEP NUMBER 44 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14760E-02 0.44972E-01 Friction velocity uk : 0.14760E-02 0.44972E-01 Dimensionless distance yplus : 0.50408E+00 0.15359E+02 Friction thermal sca. tstar : -0.97001E+01 0.16001E-01 Rough dim-less th. sca. tplus : 0.35789E+00 0.10905E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89948E-04 115 0.30881E+00 0.40777E-02 0.83239E+00 c Velocity[X] 0.70541E-03 c Velocity[Y] 0.33723E-02 c Velocity[Z] 0.66229E-29 c Pressure 0.37155E-03 11 0.37360E-07 0.62175E-01 0.17959E-02 c TempK 0.32907E+02 98 0.81422E-03 0.35879E-01 0.55899E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19684 0.21469 -7.9798e-006 -7.9798e-006 v Velocity[Y] -0.29179 0.91157 0.011796 0.011796 v Velocity[Z] -6.102e-014 6.1607e-014 -1.3774e-016 -1.3774e-016 v ǁVelocityǁ 0.00066755 0.91569 0.063425 0.063425 v Pressure -1.0107 1.0094 -7.7272e-016 -2.3852e-016 v TempK 290.84 302.99 293.84 293.84 v Density 1 1 1 1 v CourantNb 0.58591 8 7.1622 7.1622 v FourierNb 0.098079 3.1043 0.92575 0.92575 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27914 6.6264 1.9982 1.9982 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.01 303.17 293.88 293.87 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81108 11.098 8.088 8.088 INSTANT 0.450000000E+01 TIME STEP NUMBER 45 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.56429E-03 0.48648E-01 Friction velocity uk : 0.56429E-03 0.48648E-01 Dimensionless distance yplus : 0.19272E+00 0.16615E+02 Friction thermal sca. tstar : -0.19806E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.13683E+00 0.11796E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91768E-04 113 0.31146E+00 0.39554E-02 0.81711E+00 c Velocity[X] 0.70226E-03 c Velocity[Y] 0.32531E-02 c Velocity[Z] 0.63236E-29 c Pressure 0.36765E-03 11 0.35226E-07 0.63070E-01 0.18088E-02 c TempK 0.33459E+02 97 0.87844E-03 0.43090E-01 0.59353E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.25377 0.21443 2.9092e-005 2.9092e-005 v Velocity[Y] -0.32458 0.93658 0.011671 0.011671 v Velocity[Z] -6.2326e-014 6.2093e-014 -1.2372e-016 -1.2372e-016 v ǁVelocityǁ 0.00039445 0.93661 0.062669 0.062669 v Pressure -1.0077 1.0092 -1.2434e-016 5.6379e-016 v TempK 290.89 303.41 293.84 293.84 v Density 1 1 1 1 v CourantNb 0.3625 8 7.1381 7.1381 v FourierNb 0.10789 3.4148 0.91483 0.91483 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29308 7.289 1.9755 1.9755 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.84 303.15 293.89 293.88 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67828 11.289 8.0529 8.0529 INSTANT 0.460000000E+01 TIME STEP NUMBER 46 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.69673E-03 0.51187E-01 Friction velocity uk : 0.69673E-03 0.51187E-01 Dimensionless distance yplus : 0.23795E+00 0.17482E+02 Friction thermal sca. tstar : -0.15070E+02 0.83171E+00 Rough dim-less th. sca. tplus : 0.16894E+00 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.90851E-04 112 0.30236E+00 0.38544E-02 0.80096E+00 c Velocity[X] 0.72439E-03 c Velocity[Y] 0.31300E-02 c Velocity[Z] 0.65127E-29 c Pressure 0.38325E-03 11 0.34009E-07 0.64988E-01 0.16035E-02 c TempK 0.33401E+02 98 0.69071E-03 0.48324E-01 0.61115E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19781 0.19671 1.6955e-005 1.6955e-005 v Velocity[Y] -0.27367 0.88023 0.011699 0.011699 v Velocity[Z] -6.4129e-014 5.8509e-014 -1.2845e-016 -1.2845e-016 v ǁVelocityǁ 0.00019905 0.88031 0.063063 0.063063 v Pressure -1.0056 1.0093 -3.4639e-016 2.1684e-016 v TempK 291.11 304.13 293.83 293.83 v Density 1 1 1 1 v CourantNb 0.15678 8 7.057 7.057 v FourierNb 0.11868 3.7563 0.90858 0.90858 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29934 8.018 1.963 1.963 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.89 303.41 293.89 293.88 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75191 11.554 7.9655 7.9655 INSTANT 0.470000000E+01 TIME STEP NUMBER 47 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10509E-02 0.49756E-01 Friction velocity uk : 0.10509E-02 0.49756E-01 Dimensionless distance yplus : 0.35893E+00 0.16993E+02 Friction thermal sca. tstar : -0.63893E+01 0.91282E+00 Rough dim-less th. sca. tplus : 0.25483E+00 0.12065E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.90308E-04 112 0.30348E+00 0.39401E-02 0.82184E+00 c Velocity[X] 0.76569E-03 c Velocity[Y] 0.31745E-02 c Velocity[Z] 0.68718E-29 c Pressure 0.37632E-03 11 0.36384E-07 0.64817E-01 0.15770E-02 c TempK 0.33307E+02 99 0.74316E-03 0.49472E-01 0.61270E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22614 0.21054 4.7131e-005 4.7131e-005 v Velocity[Y] -0.30634 0.85426 0.0115 0.0115 v Velocity[Z] -6.48e-014 5.7833e-014 -1.3093e-016 -1.3093e-016 v ǁVelocityǁ 0.00069301 0.85522 0.062956 0.062956 v Pressure -1.0045 1.0099 -1.0303e-015 -4.0115e-016 v TempK 291.4 304.57 293.81 293.81 v Density 1 1 1 1 v CourantNb 0.30725 8 7.0631 7.0631 v FourierNb 0.13054 4.1319 0.89009 0.89009 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32315 8.8197 1.924 1.924 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.11 304.13 293.88 293.87 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57022 11.653 7.9532 7.9532 INSTANT 0.480000000E+01 TIME STEP NUMBER 48 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.80182E-03 0.45552E-01 Friction velocity uk : 0.80182E-03 0.45552E-01 Dimensionless distance yplus : 0.27385E+00 0.15557E+02 Friction thermal sca. tstar : -0.14554E+02 0.94053E+00 Rough dim-less th. sca. tplus : 0.19443E+00 0.11045E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.90643E-04 114 0.30320E+00 0.37851E-02 0.80056E+00 c Velocity[X] 0.69069E-03 c Velocity[Y] 0.30944E-02 c Velocity[Z] 0.64746E-29 c Pressure 0.34750E-03 11 0.34972E-07 0.60852E-01 0.13929E-02 c TempK 0.33333E+02 98 0.65316E-03 0.48786E-01 0.64655E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18841 0.1745 3.6216e-005 3.6216e-005 v Velocity[Y] -0.33421 0.93548 0.011544 0.011544 v Velocity[Z] -6.9113e-014 5.5309e-014 -1.2324e-016 -1.2324e-016 v ǁVelocityǁ 0.000365 0.93724 0.06298 0.06298 v Pressure -1.0056 1.0081 -7.5495e-016 -1.1926e-016 v TempK 291.59 304.96 293.8 293.8 v Density 1 1 1 1 v CourantNb 0.3446 8 7.1077 7.1077 v FourierNb 0.1436 4.5451 0.88082 0.88082 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33349 9.7017 1.9048 1.9048 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.4 304.57 293.86 293.85 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.62106 11.314 7.9885 7.9885 INSTANT 0.490000000E+01 TIME STEP NUMBER 49 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26240E-03 0.47133E-01 Friction velocity uk : 0.26240E-03 0.47133E-01 Dimensionless distance yplus : 0.89618E-01 0.16097E+02 Friction thermal sca. tstar : -0.10561E+02 0.26074E+01 Rough dim-less th. sca. tplus : 0.63627E-01 0.11429E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.93082E-04 114 0.29495E+00 0.38536E-02 0.79002E+00 c Velocity[X] 0.66521E-03 c Velocity[Y] 0.31884E-02 c Velocity[Z] 0.63271E-29 c Pressure 0.35752E-03 10 0.31266E-07 0.62086E-01 0.13720E-02 c TempK 0.33459E+02 96 0.66671E-03 0.45812E-01 0.65455E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22863 0.16723 5.1119e-005 5.1119e-005 v Velocity[Y] -0.3007 0.86245 0.011598 0.011598 v Velocity[Z] -6.8783e-014 5.9658e-014 -1.3862e-016 -1.3862e-016 v ǁVelocityǁ 0.00019075 0.86275 0.063622 0.063622 v Pressure -1.0073 1.007 -8.8818e-018 5.7463e-016 v TempK 291.64 305.47 293.8 293.8 v Density 1 1 1 1 v CourantNb 0.36913 8 7.0999 7.0999 v FourierNb 0.12035 4.7974 0.87442 0.87442 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31012 10.24 1.8926 1.8926 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.59 304.96 293.85 293.84 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69124 12.797 7.9744 7.9744 INSTANT 0.500000000E+01 TIME STEP NUMBER 50 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.70165E-03 0.47122E-01 Friction velocity uk : 0.70165E-03 0.47122E-01 Dimensionless distance yplus : 0.23964E+00 0.16093E+02 Friction thermal sca. tstar : -0.13121E+02 0.20176E+01 Rough dim-less th. sca. tplus : 0.17014E+00 0.11426E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94484E-04 113 0.30611E+00 0.39547E-02 0.81104E+00 c Velocity[X] 0.73393E-03 c Velocity[Y] 0.32208E-02 c Velocity[Z] 0.67055E-29 c Pressure 0.36460E-03 10 0.33274E-07 0.62715E-01 0.14574E-02 c TempK 0.33803E+02 94 0.57014E-03 0.42952E-01 0.65419E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24606 0.21273 2.7582e-005 2.7582e-005 v Velocity[Y] -0.26481 0.89838 0.011424 0.011424 v Velocity[Z] -6.4876e-014 5.6753e-014 -1.4923e-016 -1.4923e-016 v ǁVelocityǁ 0.00019443 0.90272 0.06345 0.06345 v Pressure -1.0077 1.0067 1.2434e-016 7.8063e-016 v TempK 291.55 305.14 293.81 293.81 v Density 1 1 1 1 v CourantNb 0.21532 8 7.1024 7.1024 v FourierNb 0.12276 4.492 0.87147 0.87147 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29218 10.304 1.8874 1.8874 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.64 305.47 293.85 293.84 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.44388 11.626 7.9739 7.9739 INSTANT 0.510000000E+01 TIME STEP NUMBER 51 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.33266E-03 0.43284E-01 Friction velocity uk : 0.33266E-03 0.43284E-01 Dimensionless distance yplus : 0.11361E+00 0.14783E+02 Friction thermal sca. tstar : -0.25462E+02 0.10909E+01 Rough dim-less th. sca. tplus : 0.80664E-01 0.10495E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.90960E-04 115 0.29766E+00 0.38649E-02 0.79189E+00 c Velocity[X] 0.71976E-03 c Velocity[Y] 0.31451E-02 c Velocity[Z] 0.68596E-29 c Pressure 0.36758E-03 12 0.32389E-07 0.67446E-01 0.15378E-02 c TempK 0.33843E+02 93 0.89971E-03 0.39820E-01 0.64172E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24037 0.19695 4.9648e-005 4.9648e-005 v Velocity[Y] -0.28929 0.84323 0.011461 0.011461 v Velocity[Z] -7.4965e-014 6.1032e-014 -1.6298e-016 -1.6298e-016 v ǁVelocityǁ 0.00084113 0.85217 0.063808 0.063808 v Pressure -1.0093 1.0082 2.6645e-016 8.9989e-016 v TempK 291.16 305.23 293.83 293.83 v Density 1 1 1 1 v CourantNb 0.45558 8 7.1163 7.1163 v FourierNb 0.13503 3.9824 0.86914 0.86914 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30803 11.334 1.8812 1.8812 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.55 305.14 293.86 293.85 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.78013 11.315 7.9855 7.9855 INSTANT 0.520000000E+01 TIME STEP NUMBER 52 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.96242E-03 0.44814E-01 Friction velocity uk : 0.96242E-03 0.44814E-01 Dimensionless distance yplus : 0.32869E+00 0.15305E+02 Friction thermal sca. tstar : -0.40225E+01 0.31354E+01 Rough dim-less th. sca. tplus : 0.23337E+00 0.10866E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.92287E-04 112 0.30522E+00 0.39245E-02 0.80118E+00 c Velocity[X] 0.68998E-03 c Velocity[Y] 0.32345E-02 c Velocity[Z] 0.64983E-29 c Pressure 0.35834E-03 11 0.36116E-07 0.64855E-01 0.16227E-02 c TempK 0.34062E+02 93 0.58189E-03 0.35275E-01 0.62710E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23857 0.18932 3.5752e-005 3.5752e-005 v Velocity[Y] -0.34519 0.87504 0.011652 0.011652 v Velocity[Z] -6.129e-014 5.9756e-014 -1.4006e-016 -1.4006e-016 v ǁVelocityǁ 0.00014125 0.88646 0.064022 0.064022 v Pressure -1.0098 1.0064 -7.7272e-016 -1.7347e-016 v TempK 290.53 305.06 293.85 293.85 v Density 1 1 1 1 v CourantNb 0.2531 8 7.1337 7.1337 v FourierNb 0.1315 4.3807 0.87276 0.87276 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29628 12.468 1.8899 1.8899 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.16 305.23 293.88 293.87 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.51779 11.849 8.0064 8.0064 INSTANT 0.530000000E+01 TIME STEP NUMBER 53 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10249E-02 0.45033E-01 Friction velocity uk : 0.10249E-02 0.45033E-01 Dimensionless distance yplus : 0.35004E+00 0.15380E+02 Friction thermal sca. tstar : -0.66555E+01 0.11749E+01 Rough dim-less th. sca. tplus : 0.24852E+00 0.10920E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.95132E-04 112 0.30387E+00 0.39407E-02 0.81118E+00 c Velocity[X] 0.65676E-03 c Velocity[Y] 0.32839E-02 c Velocity[Z] 0.61020E-29 c Pressure 0.36451E-03 11 0.33869E-07 0.64623E-01 0.16481E-02 c TempK 0.34106E+02 93 0.74459E-03 0.32553E-01 0.61393E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19208 0.17776 2.9154e-005 2.9154e-005 v Velocity[Y] -0.32055 1.0185 0.011625 0.011625 v Velocity[Z] -6.4037e-014 5.9672e-014 -1.355e-016 -1.355e-016 v ǁVelocityǁ 0.00055916 1.0186 0.063698 0.063698 v Pressure -1.0077 1.007 -3.0198e-016 2.6021e-016 v TempK 289.84 304.88 293.87 293.87 v Density 1 1 1 1 v CourantNb 0.12799 8 7.0904 7.0904 v FourierNb 0.11104 4.8187 0.87885 0.87885 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28778 13.714 1.9038 1.9038 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.53 305.06 293.9 293.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57557 11.666 7.9692 7.9692 INSTANT 0.540000000E+01 TIME STEP NUMBER 54 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.40579E-03 0.49701E-01 Friction velocity uk : 0.40579E-03 0.49701E-01 Dimensionless distance yplus : 0.13859E+00 0.16974E+02 Friction thermal sca. tstar : -0.84299E+01 0.16531E+01 Rough dim-less th. sca. tplus : 0.98396E-01 0.12052E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.88074E-04 113 0.28369E+00 0.35527E-02 0.74787E+00 c Velocity[X] 0.67683E-03 c Velocity[Y] 0.28759E-02 c Velocity[Z] 0.54190E-29 c Pressure 0.38566E-03 10 0.30745E-07 0.68611E-01 0.14323E-02 c TempK 0.33700E+02 93 0.76233E-03 0.27715E-01 0.57036E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21789 0.19625 1.9046e-006 1.9046e-006 v Velocity[Y] -0.27598 0.84622 0.011634 0.011634 v Velocity[Z] -5.9035e-014 5.5902e-014 -1.509e-016 -1.509e-016 v ǁVelocityǁ 0.00030376 0.848 0.064166 0.064166 v Pressure -1.0072 1.0063 -5.7732e-016 4.3368e-017 v TempK 289.53 304.38 293.89 293.89 v Density 1 1 1 1 v CourantNb 0.28898 8 7.0626 7.0626 v FourierNb 0.12215 4.2303 0.88838 0.88838 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31656 11.783 1.9248 1.9248 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 289.84 304.88 293.92 293.91 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.53167 12.2 7.951 7.951 INSTANT 0.550000000E+01 TIME STEP NUMBER 55 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.78587E-03 0.44208E-01 Friction velocity uk : 0.78587E-03 0.44208E-01 Dimensionless distance yplus : 0.26840E+00 0.15098E+02 Friction thermal sca. tstar : -0.69161E+01 0.11799E+01 Rough dim-less th. sca. tplus : 0.19056E+00 0.10720E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89404E-04 113 0.29309E+00 0.37387E-02 0.78588E+00 c Velocity[X] 0.70588E-03 c Velocity[Y] 0.30328E-02 c Velocity[Z] 0.56805E-29 c Pressure 0.36552E-03 10 0.32555E-07 0.64061E-01 0.15263E-02 c TempK 0.33609E+02 92 0.83191E-03 0.24891E-01 0.52239E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.25839 0.19099 2.8892e-005 2.8892e-005 v Velocity[Y] -0.29433 0.91564 0.011432 0.011432 v Velocity[Z] -5.8972e-014 6.2571e-014 -1.3167e-016 -1.3167e-016 v ǁVelocityǁ 6.8654e-005 0.92487 0.063997 0.063997 v Pressure -1.0065 1.0082 3.1974e-016 8.6736e-016 v TempK 289.74 303.89 293.91 293.91 v Density 1 1 1 1 v CourantNb 0.24804 8 7.0835 7.0835 v FourierNb 0.13436 4.6533 0.90248 0.90248 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32535 12.961 1.9561 1.9561 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 289.53 304.38 293.94 293.93 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.51014 11.896 7.986 7.986 INSTANT 0.560000000E+01 TIME STEP NUMBER 56 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.93532E-03 0.47208E-01 Friction velocity uk : 0.93532E-03 0.47208E-01 Dimensionless distance yplus : 0.31944E+00 0.16123E+02 Friction thermal sca. tstar : -0.45614E+01 0.25506E+01 Rough dim-less th. sca. tplus : 0.22680E+00 0.11447E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87988E-04 113 0.29968E+00 0.37169E-02 0.78101E+00 c Velocity[X] 0.65242E-03 c Velocity[Y] 0.30645E-02 c Velocity[Z] 0.62769E-29 c Pressure 0.35101E-03 10 0.30304E-07 0.59228E-01 0.13776E-02 c TempK 0.33663E+02 93 0.66018E-03 0.21279E-01 0.49043E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19865 0.20483 -8.8776e-007 -8.8776e-007 v Velocity[Y] -0.24473 0.87852 0.011497 0.011497 v Velocity[Z] -5.9305e-014 6.8732e-014 -1.3228e-016 -1.3228e-016 v ǁVelocityǁ 0.00032923 0.8814 0.064739 0.064739 v Pressure -1.0065 1.007 -2.0073e-015 -1.4637e-015 v TempK 290.23 303.96 293.92 293.92 v Density 1 1 1 1 v CourantNb 0.26727 8 7.0367 7.0367 v FourierNb 0.11862 5.1186 0.92194 0.92194 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27626 14.257 1.999 1.999 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 289.74 303.89 293.96 293.95 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.66003 12.072 7.9586 7.9586 INSTANT 0.570000000E+01 TIME STEP NUMBER 57 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.22812E-03 0.43391E-01 Friction velocity uk : 0.22812E-03 0.43391E-01 Dimensionless distance yplus : 0.77910E-01 0.14819E+02 Friction thermal sca. tstar : -0.23089E+02 0.67558E+00 Rough dim-less th. sca. tplus : 0.55315E-01 0.10521E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87463E-04 116 0.28165E+00 0.36622E-02 0.75869E+00 c Velocity[X] 0.66228E-03 c Velocity[Y] 0.30000E-02 c Velocity[Z] 0.59000E-29 c Pressure 0.35881E-03 10 0.31305E-07 0.59550E-01 0.14040E-02 c TempK 0.33704E+02 95 0.83892E-03 0.20182E-01 0.47072E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24654 0.21158 1.9346e-005 1.9346e-005 v Velocity[Y] -0.24952 0.95221 0.011545 0.011545 v Velocity[Z] -6.1096e-014 6.9826e-014 -1.3299e-016 -1.3299e-016 v ǁVelocityǁ 7.5155e-005 0.955 0.065413 0.065413 v Pressure -1.0052 1.0085 -5.4179e-016 3.2526e-017 v TempK 290.69 304.35 293.95 293.95 v Density 1 1 1 1 v CourantNb 0.27446 8 7.0951 7.0951 v FourierNb 0.13048 5.6305 0.93511 0.93511 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30389 15.683 2.0283 2.0283 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.23 303.96 293.98 293.97 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.6617 12.876 8.0302 8.0302 INSTANT 0.580000000E+01 TIME STEP NUMBER 58 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.67381E-03 0.43947E-01 Friction velocity uk : 0.67381E-03 0.43947E-01 Dimensionless distance yplus : 0.23013E+00 0.15009E+02 Friction thermal sca. tstar : -0.88526E+01 0.94593E+00 Rough dim-less th. sca. tplus : 0.16339E+00 0.10656E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87090E-04 116 0.29007E+00 0.37897E-02 0.78086E+00 c Velocity[X] 0.68539E-03 c Velocity[Y] 0.31043E-02 c Velocity[Z] 0.57950E-29 c Pressure 0.35840E-03 10 0.29656E-07 0.61255E-01 0.15619E-02 c TempK 0.33845E+02 95 0.68962E-03 0.17615E-01 0.43702E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.2027 0.18063 1.0412e-005 1.0412e-005 v Velocity[Y] -0.22282 0.98838 0.011281 0.011281 v Velocity[Z] -6.9823e-014 6.706e-014 -1.2855e-016 -1.2855e-016 v ǁVelocityǁ 0.00038129 0.98992 0.065897 0.065897 v Pressure -1.004 1.0071 9.1482e-016 1.4962e-015 v TempK 291.03 304.65 293.98 293.98 v Density 1 1 1 1 v CourantNb 0.28975 8 7.1241 7.1241 v FourierNb 0.12559 5.4814 0.93192 0.93192 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26807 13.556 2.0202 2.0202 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.69 304.35 294 293.99 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85269 12.513 8.056 8.056 INSTANT 0.590000000E+01 TIME STEP NUMBER 59 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11458E-02 0.43816E-01 Friction velocity uk : 0.11458E-02 0.43816E-01 Dimensionless distance yplus : 0.39132E+00 0.14964E+02 Friction thermal sca. tstar : -0.53771E+01 0.25728E+01 Rough dim-less th. sca. tplus : 0.27783E+00 0.10624E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85197E-04 114 0.28695E+00 0.33217E-02 0.72002E+00 c Velocity[X] 0.62155E-03 c Velocity[Y] 0.27001E-02 c Velocity[Z] 0.62243E-29 c Pressure 0.34747E-03 11 0.28632E-07 0.59140E-01 0.12580E-02 c TempK 0.33940E+02 96 0.83417E-03 0.15782E-01 0.40615E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20184 0.18748 5.8472e-006 5.8472e-006 v Velocity[Y] -0.24873 0.84352 0.011545 0.011545 v Velocity[Z] -6.217e-014 6.9475e-014 -1.1984e-016 -1.1984e-016 v ǁVelocityǁ 0.00022566 0.84368 0.066893 0.066893 v Pressure -1.0036 1.0065 2.3093e-016 8.3484e-016 v TempK 291.3 305.56 294.01 294.01 v Density 1 1 1 1 v CourantNb 0.18827 8 7.1866 7.1866 v FourierNb 0.13814 4.5443 0.91667 0.91667 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29488 12.461 1.9854 1.9854 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.03 304.65 294.03 294.02 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.56282 12.262 8.1032 8.1032 INSTANT 0.600000000E+01 TIME STEP NUMBER 60 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.19140E-03 0.44784E-01 Friction velocity uk : 0.19140E-03 0.44784E-01 Dimensionless distance yplus : 0.65371E-01 0.15295E+02 Friction thermal sca. tstar : -0.37781E+01 0.16450E+01 Rough dim-less th. sca. tplus : 0.46412E-01 0.10859E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82352E-04 116 0.28588E+00 0.33910E-02 0.70424E+00 c Velocity[X] 0.63793E-03 c Velocity[Y] 0.27531E-02 c Velocity[Z] 0.59569E-29 c Pressure 0.36617E-03 11 0.29952E-07 0.60486E-01 0.13094E-02 c TempK 0.33952E+02 93 0.62657E-03 0.14928E-01 0.38278E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16821 0.19473 -1.7277e-005 -1.7277e-005 v Velocity[Y] -0.25235 1.0006 0.011846 0.011846 v Velocity[Z] -5.1977e-014 6.8582e-014 -1.1594e-016 -1.1594e-016 v ǁVelocityǁ 0.00063931 1.0059 0.067722 0.067722 v Pressure -1.0034 1.0068 2.4869e-016 8.5652e-016 v TempK 291.54 306.07 294.03 294.03 v Density 1 1 1 1 v CourantNb 0.34816 8 7.2467 7.2467 v FourierNb 0.15196 4.3416 0.89132 0.89132 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32436 12.356 1.9304 1.9304 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.3 305.56 294.06 294.05 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.58176 12.277 8.138 8.138 INSTANT 0.610000000E+01 TIME STEP NUMBER 61 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.81683E-03 0.46100E-01 Friction velocity uk : 0.81683E-03 0.46100E-01 Dimensionless distance yplus : 0.27897E+00 0.15744E+02 Friction thermal sca. tstar : -0.68701E+01 0.16999E+01 Rough dim-less th. sca. tplus : 0.19807E+00 0.11178E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85875E-04 115 0.29469E+00 0.34626E-02 0.71686E+00 c Velocity[X] 0.65995E-03 c Velocity[Y] 0.28026E-02 c Velocity[Z] 0.50533E-29 c Pressure 0.37251E-03 14 0.31525E-07 0.62552E-01 0.12897E-02 c TempK 0.34164E+02 91 0.70994E-03 0.12927E-01 0.36179E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21059 0.21739 5.5114e-006 5.5114e-006 v Velocity[Y] -0.34342 0.90916 0.011785 0.011785 v Velocity[Z] -5.3984e-014 6.6958e-014 -1.0415e-016 -1.0415e-016 v ǁVelocityǁ 0.00050967 0.90916 0.068129 0.068129 v Pressure -1.0049 1.008 -8.793e-016 -2.6021e-016 v TempK 291.78 305.87 294.06 294.06 v Density 1 1 1 1 v CourantNb 0.66708 8 7.2712 7.2712 v FourierNb 0.14835 4.7757 0.87431 0.87431 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31667 13.592 1.8943 1.8943 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.54 306.07 294.09 294.08 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0575 12.682 8.1456 8.1456 INSTANT 0.620000000E+01 TIME STEP NUMBER 62 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.49067E-03 0.45124E-01 Friction velocity uk : 0.49067E-03 0.45124E-01 Dimensionless distance yplus : 0.16758E+00 0.15411E+02 Friction thermal sca. tstar : -0.33637E+01 0.18958E+01 Rough dim-less th. sca. tplus : 0.11898E+00 0.10942E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.84468E-04 115 0.29083E+00 0.34615E-02 0.72211E+00 c Velocity[X] 0.63945E-03 c Velocity[Y] 0.28221E-02 c Velocity[Z] 0.53492E-29 c Pressure 0.35297E-03 11 0.35011E-07 0.59159E-01 0.13121E-02 c TempK 0.34460E+02 91 0.60137E-03 0.12867E-01 0.36210E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22071 0.20755 -1.5266e-005 -1.5266e-005 v Velocity[Y] -0.30706 1.0853 0.011532 0.011532 v Velocity[Z] -6.1548e-014 6.5126e-014 -1.1253e-016 -1.1253e-016 v ǁVelocityǁ 0.0010293 1.0853 0.068719 0.068719 v Pressure -1.0062 1.0063 -1.7764e-017 5.3126e-016 v TempK 292.03 306.19 294.08 294.08 v Density 1 1 1 1 v CourantNb 0.35932 8 7.2873 7.2873 v FourierNb 0.13592 4.5943 0.86682 0.86682 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29012 13.076 1.8781 1.8781 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.78 305.87 294.11 294.1 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.53775 12.361 8.1542 8.1542 INSTANT 0.630000000E+01 TIME STEP NUMBER 63 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.83987E-03 0.44484E-01 Friction velocity uk : 0.83987E-03 0.44484E-01 Dimensionless distance yplus : 0.28684E+00 0.15193E+02 Friction thermal sca. tstar : -0.39256E+01 0.35447E+01 Rough dim-less th. sca. tplus : 0.20365E+00 0.10787E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81765E-04 115 0.28231E+00 0.32165E-02 0.67698E+00 c Velocity[X] 0.60701E-03 c Velocity[Y] 0.26094E-02 c Velocity[Z] 0.48962E-29 c Pressure 0.35083E-03 10 0.36255E-07 0.60907E-01 0.13624E-02 c TempK 0.34660E+02 91 0.70208E-03 0.13361E-01 0.38040E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19537 0.22096 8.5967e-006 8.5967e-006 v Velocity[Y] -0.28887 1.3673 0.011745 0.011745 v Velocity[Z] -6.3949e-014 6.0278e-014 -1.0898e-016 -1.0898e-016 v ǁVelocityǁ 0.00053116 1.3673 0.069496 0.069496 v Pressure -1.0059 1.0081 -1.0658e-015 -4.6621e-016 v TempK 292.17 305.78 294.1 294.1 v Density 1 1 1 1 v CourantNb 0.36528 8 7.356 7.356 v FourierNb 0.14277 5.0283 0.853 0.853 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3186 14.311 1.8495 1.8495 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.03 306.19 294.13 294.12 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.74527 12.082 8.209 8.209 INSTANT 0.640000000E+01 TIME STEP NUMBER 64 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.24481E-03 0.44452E-01 Friction velocity uk : 0.24481E-03 0.44452E-01 Dimensionless distance yplus : 0.83611E-01 0.15182E+02 Friction thermal sca. tstar : -0.20381E+02 0.32793E+02 Rough dim-less th. sca. tplus : 0.59362E-01 0.10779E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81148E-04 115 0.29060E+00 0.34441E-02 0.69623E+00 c Velocity[X] 0.58389E-03 c Velocity[Y] 0.28602E-02 c Velocity[Z] 0.52188E-29 c Pressure 0.36125E-03 11 0.35695E-07 0.63329E-01 0.12690E-02 c TempK 0.35061E+02 90 0.57536E-03 0.14151E-01 0.39480E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20727 0.22136 -6.5049e-006 -6.5049e-006 v Velocity[Y] -0.25804 1.0136 0.011942 0.011942 v Velocity[Z] -5.8765e-014 6.0571e-014 -1.2516e-016 -1.2516e-016 v ǁVelocityǁ 0.00056436 1.0139 0.069616 0.069616 v Pressure -1.0056 1.008 -4.2633e-016 2.06e-016 v TempK 292.13 305.63 294.12 294.12 v Density 1 1 1 1 v CourantNb 0.32102 8 7.3339 7.3339 v FourierNb 0.1348 5.5311 0.83287 0.83287 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29496 15.742 1.8077 1.8077 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.17 305.78 294.15 294.14 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72522 13.364 8.1667 8.1667 INSTANT 0.650000000E+01 TIME STEP NUMBER 65 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.92604E-03 0.45605E-01 Friction velocity uk : 0.92604E-03 0.45605E-01 Dimensionless distance yplus : 0.31627E+00 0.15575E+02 Friction thermal sca. tstar : -0.44426E+01 0.31309E+01 Rough dim-less th. sca. tplus : 0.22455E+00 0.11058E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85296E-04 113 0.29919E+00 0.36375E-02 0.72447E+00 c Velocity[X] 0.59034E-03 c Velocity[Y] 0.30471E-02 c Velocity[Z] 0.55219E-29 c Pressure 0.39256E-03 11 0.36614E-07 0.68963E-01 0.13864E-02 c TempK 0.35400E+02 91 0.76050E-03 0.14915E-01 0.41049E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18384 0.19554 1.312e-005 1.312e-005 v Velocity[Y] -0.35667 0.93951 0.01179 0.01179 v Velocity[Z] -6.0368e-014 5.6787e-014 -1.1392e-016 -1.1392e-016 v ǁVelocityǁ 0.00049002 0.93985 0.070023 0.070023 v Pressure -1.0047 1.0072 -1.5987e-015 -9.7578e-016 v TempK 291.95 305.06 294.14 294.14 v Density 1 1 1 1 v CourantNb 0.19221 8 7.3037 7.3037 v FourierNb 0.14828 5.4803 0.82141 0.82141 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31707 15.598 1.7824 1.7824 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.13 305.63 294.17 294.16 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85865 13.48 8.1251 8.1251 INSTANT 0.660000000E+01 TIME STEP NUMBER 66 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.53798E-04 0.46475E-01 Friction velocity uk : 0.53798E-04 0.46475E-01 Dimensionless distance yplus : 0.18373E-01 0.15873E+02 Friction thermal sca. tstar : -0.75421E+01 0.51301E+01 Rough dim-less th. sca. tplus : 0.13045E-01 0.11269E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89169E-04 112 0.31194E+00 0.36182E-02 0.75501E+00 c Velocity[X] 0.63734E-03 c Velocity[Y] 0.29809E-02 c Velocity[Z] 0.54023E-29 c Pressure 0.38196E-03 10 0.33872E-07 0.67277E-01 0.12802E-02 c TempK 0.35741E+02 92 0.65475E-03 0.19932E-01 0.47191E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18152 0.2165 9.3615e-006 9.3615e-006 v Velocity[Y] -0.35249 0.90641 0.011505 0.011505 v Velocity[Z] -6.2901e-014 5.836e-014 -1.2839e-016 -1.2839e-016 v ǁVelocityǁ 9.8107e-005 0.90651 0.069662 0.069662 v Pressure -1.0042 1.0064 -6.9278e-016 -4.3368e-017 v TempK 291.72 304.62 294.16 294.16 v Density 1 1 1 1 v CourantNb 0.35882 8 7.3282 7.3282 v FourierNb 0.11907 5.4065 0.81241 0.81241 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31338 15.387 1.7617 1.7617 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.95 305.06 294.19 294.18 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.88247 12.553 8.1406 8.1406 INSTANT 0.670000000E+01 TIME STEP NUMBER 67 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26549E-03 0.44552E-01 Friction velocity uk : 0.26549E-03 0.44552E-01 Dimensionless distance yplus : 0.90672E-01 0.15216E+02 Friction thermal sca. tstar : -0.55925E+01 0.11452E+01 Rough dim-less th. sca. tplus : 0.64375E-01 0.10803E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85106E-04 113 0.30876E+00 0.34127E-02 0.72362E+00 c Velocity[X] 0.60538E-03 c Velocity[Y] 0.28074E-02 c Velocity[Z] 0.57075E-29 c Pressure 0.36515E-03 10 0.32935E-07 0.63098E-01 0.14141E-02 c TempK 0.35776E+02 93 0.77927E-03 0.30341E-01 0.57434E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17634 0.25036 4.7121e-006 4.7121e-006 v Velocity[Y] -0.3248 0.95015 0.011487 0.011487 v Velocity[Z] -5.6664e-014 5.5192e-014 -1.3025e-016 -1.3025e-016 v ǁVelocityǁ 9.6374e-005 0.95025 0.06993 0.06993 v Pressure -1.0048 1.0071 4.2633e-016 9.9747e-016 v TempK 291.49 303.48 294.19 294.19 v Density 1 1 1 1 v CourantNb 0.27861 8 7.2803 7.2803 v FourierNb 0.12853 5.9471 0.80533 0.80533 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28613 16.926 1.7471 1.7471 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.72 304.62 294.22 294.21 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.70754 12.548 8.0856 8.0856 INSTANT 0.680000000E+01 TIME STEP NUMBER 68 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.67039E-03 0.42583E-01 Friction velocity uk : 0.67039E-03 0.42583E-01 Dimensionless distance yplus : 0.22896E+00 0.14544E+02 Friction thermal sca. tstar : -0.39951E+01 0.12672E+01 Rough dim-less th. sca. tplus : 0.16256E+00 0.10326E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81384E-04 114 0.30686E+00 0.33637E-02 0.71713E+00 c Velocity[X] 0.61218E-03 c Velocity[Y] 0.27515E-02 c Velocity[Z] 0.55624E-29 c Pressure 0.36963E-03 11 0.31573E-07 0.64008E-01 0.14063E-02 c TempK 0.35802E+02 95 0.61582E-03 0.31445E-01 0.58752E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22552 0.20236 -8.2246e-006 -8.2246e-006 v Velocity[Y] -0.28153 0.92158 0.011508 0.011508 v Velocity[Z] -5.9495e-014 5.3881e-014 -1.454e-016 -1.454e-016 v ǁVelocityǁ 0.00019532 0.9221 0.069898 0.069898 v Pressure -1.0044 1.0076 -2.1938e-015 -1.5504e-015 v TempK 291.35 303.02 294.21 294.21 v Density 1 1 1 1 v CourantNb 0.34584 8 7.3609 7.3609 v FourierNb 0.13141 5.2163 0.79594 0.79594 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2805 14.846 1.7258 1.7258 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.49 303.48 294.24 294.23 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85955 12.654 8.1569 8.1569 INSTANT 0.690000000E+01 TIME STEP NUMBER 69 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.84459E-03 0.43183E-01 Friction velocity uk : 0.84459E-03 0.43183E-01 Dimensionless distance yplus : 0.28845E+00 0.14748E+02 Friction thermal sca. tstar : -0.50467E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.20480E+00 0.10471E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81282E-04 115 0.30226E+00 0.33409E-02 0.70766E+00 c Velocity[X] 0.58843E-03 c Velocity[Y] 0.27525E-02 c Velocity[Z] 0.52736E-29 c Pressure 0.36002E-03 11 0.35254E-07 0.60356E-01 0.14824E-02 c TempK 0.35890E+02 96 0.69461E-03 0.33867E-01 0.61035E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19774 0.22925 1.1142e-005 1.1142e-005 v Velocity[Y] -0.27643 0.87597 0.011764 0.011764 v Velocity[Z] -5.1695e-014 5.56e-014 -1.2586e-016 -1.2586e-016 v ǁVelocityǁ 0.00020231 0.89114 0.070562 0.070562 v Pressure -1.0062 1.006 -6.3949e-016 -7.5894e-017 v TempK 291.31 302.8 294.22 294.22 v Density 1 1 1 1 v CourantNb 0.67179 8 7.2895 7.2895 v FourierNb 0.14144 5.738 0.79279 0.79279 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30191 16.331 1.7191 1.7191 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.35 303.15 294.26 294.25 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0961 12.532 8.0823 8.0823 INSTANT 0.700000000E+01 TIME STEP NUMBER 70 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.82938E-03 0.42260E-01 Friction velocity uk : 0.82938E-03 0.42260E-01 Dimensionless distance yplus : 0.28326E+00 0.14433E+02 Friction thermal sca. tstar : -0.10324E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.20111E+00 0.10247E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79210E-04 115 0.29632E+00 0.33391E-02 0.69800E+00 c Velocity[X] 0.63348E-03 c Velocity[Y] 0.27056E-02 c Velocity[Z] 0.52962E-29 c Pressure 0.37357E-03 15 0.31148E-07 0.62641E-01 0.13938E-02 c TempK 0.35981E+02 96 0.59454E-03 0.37411E-01 0.63529E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15517 0.22556 1.0849e-005 1.0849e-005 v Velocity[Y] -0.26823 1.0166 0.011694 0.011694 v Velocity[Z] -5.6721e-014 5.7205e-014 -1.2112e-016 -1.2112e-016 v ǁVelocityǁ 0.00036589 1.0168 0.070392 0.070392 v Pressure -1.0052 1.0076 2.931e-016 8.6736e-016 v TempK 291.36 302.99 294.25 294.25 v Density 1 1 1 1 v CourantNb 0.1969 8 7.2861 7.2861 v FourierNb 0.14905 5.631 0.78553 0.78553 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32913 14.944 1.7039 1.7039 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.31 303.15 294.28 294.27 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85295 12.325 8.0717 8.0717 INSTANT 0.710000000E+01 TIME STEP NUMBER 71 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.82674E-04 0.42846E-01 Friction velocity uk : 0.82674E-04 0.42846E-01 Dimensionless distance yplus : 0.28236E-01 0.14633E+02 Friction thermal sca. tstar : -0.61402E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.20047E-01 0.10389E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83228E-04 115 0.29635E+00 0.34843E-02 0.72160E+00 c Velocity[X] 0.63090E-03 c Velocity[Y] 0.28534E-02 c Velocity[Z] 0.57716E-29 c Pressure 0.36894E-03 10 0.37192E-07 0.60852E-01 0.14607E-02 c TempK 0.36077E+02 94 0.67007E-03 0.40816E-01 0.65391E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17762 0.22046 2.7802e-005 2.7802e-005 v Velocity[Y] -0.25053 1.0481 0.011495 0.011495 v Velocity[Z] -5.2484e-014 4.9608e-014 -1.2083e-016 -1.2083e-016 v ǁVelocityǁ 0.00048612 1.0481 0.07017 0.07017 v Pressure -1.0059 1.0061 -7.2831e-016 -1.6263e-016 v TempK 291.44 303.45 294.27 294.27 v Density 1 1 1 1 v CourantNb 0.26214 8 7.2463 7.2463 v FourierNb 0.14393 6.0869 0.7803 0.7803 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31675 15.551 1.6939 1.6939 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.36 303.15 294.3 294.29 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.86577 13.178 8.0266 8.0266 INSTANT 0.720000000E+01 TIME STEP NUMBER 72 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.72051E-03 0.42311E-01 Friction velocity uk : 0.72051E-03 0.42311E-01 Dimensionless distance yplus : 0.24608E+00 0.14450E+02 Friction thermal sca. tstar : -0.11949E+02 0.12277E+01 Rough dim-less th. sca. tplus : 0.17471E+00 0.10260E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83176E-04 114 0.29017E+00 0.35402E-02 0.73388E+00 c Velocity[X] 0.64063E-03 c Velocity[Y] 0.28996E-02 c Velocity[Z] 0.57739E-29 c Pressure 0.36574E-03 11 0.34059E-07 0.58600E-01 0.15273E-02 c TempK 0.36034E+02 94 0.55041E-03 0.39207E-01 0.65512E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1432 0.22044 -1.6248e-006 -1.6248e-006 v Velocity[Y] -0.31046 0.93766 0.011363 0.011363 v Velocity[Z] -4.704e-014 5.5217e-014 -1.3732e-016 -1.3732e-016 v ǁVelocityǁ 0.00028771 0.94027 0.070533 0.070533 v Pressure -1.0044 1.0072 -3.2863e-016 2.6021e-016 v TempK 291.54 304.07 294.3 294.3 v Density 1 1 1 1 v CourantNb 0.49497 8 7.273 7.273 v FourierNb 0.13141 6.401 0.78356 0.78356 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2805 17.106 1.7018 1.7018 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.44 303.45 294.33 294.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0111 14.234 8.0566 8.0566 INSTANT 0.730000000E+01 TIME STEP NUMBER 73 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.25449E-03 0.41494E-01 Friction velocity uk : 0.25449E-03 0.41494E-01 Dimensionless distance yplus : 0.86915E-01 0.14171E+02 Friction thermal sca. tstar : -0.67927E+01 0.14415E+01 Rough dim-less th. sca. tplus : 0.61708E-01 0.10061E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82961E-04 115 0.28781E+00 0.32707E-02 0.70711E+00 c Velocity[X] 0.56771E-03 c Velocity[Y] 0.27030E-02 c Velocity[Z] 0.60192E-29 c Pressure 0.34203E-03 11 0.34424E-07 0.52586E-01 0.14852E-02 c TempK 0.36069E+02 93 0.68032E-03 0.34855E-01 0.61760E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1452 0.19464 3.2903e-005 3.2903e-005 v Velocity[Y] -0.21334 0.94501 0.011577 0.011577 v Velocity[Z] -5.326e-014 4.7602e-014 -1.2199e-016 -1.2199e-016 v ǁVelocityǁ 0.00019575 0.94509 0.070661 0.070661 v Pressure -1.0044 1.0057 -1.3145e-015 -7.1557e-016 v TempK 291.66 304.57 294.32 294.32 v Density 1 1 1 1 v CourantNb 0.26098 8 7.2768 7.2768 v FourierNb 0.13384 7.0411 0.78713 0.78713 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2857 18.816 1.7105 1.7105 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.54 304.07 294.35 294.34 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67538 14.265 8.0639 8.0639 INSTANT 0.740000000E+01 TIME STEP NUMBER 74 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.43890E-03 0.41253E-01 Friction velocity uk : 0.43890E-03 0.41253E-01 Dimensionless distance yplus : 0.14990E+00 0.14089E+02 Friction thermal sca. tstar : -0.10495E+02 0.21346E+01 Rough dim-less th. sca. tplus : 0.10643E+00 0.10003E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81886E-04 115 0.29286E+00 0.32019E-02 0.66043E+00 c Velocity[X] 0.54477E-03 c Velocity[Y] 0.26571E-02 c Velocity[Z] 0.59991E-29 c Pressure 0.35820E-03 10 0.28152E-07 0.54838E-01 0.12681E-02 c TempK 0.35901E+02 93 0.54837E-03 0.31634E-01 0.59611E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23675 0.17922 7.4419e-006 7.4419e-006 v Velocity[Y] -0.24726 1.1173 0.012057 0.012057 v Velocity[Z] -4.8988e-014 5.19e-014 -1.403e-016 -1.403e-016 v ǁVelocityǁ 0.00092384 1.1177 0.071137 0.071137 v Pressure -1.005 1.0056 -9.3259e-016 -3.2526e-016 v TempK 291.75 304.81 294.34 294.34 v Density 1 1 1 1 v CourantNb 0.052037 8 7.2662 7.2662 v FourierNb 0.14723 7.2724 0.78867 0.78867 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31427 20.698 1.7139 1.7139 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.66 304.57 294.37 294.36 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.71872 15.189 8.0549 8.0549 INSTANT 0.750000000E+01 TIME STEP NUMBER 75 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32693E-03 0.45718E-01 Friction velocity uk : 0.32693E-03 0.45718E-01 Dimensionless distance yplus : 0.11166E+00 0.15614E+02 Friction thermal sca. tstar : -0.23894E+02 0.37627E+01 Rough dim-less th. sca. tplus : 0.79275E-01 0.11086E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89005E-04 114 0.32916E+00 0.36191E-02 0.72533E+00 c Velocity[X] 0.59231E-03 c Velocity[Y] 0.30268E-02 c Velocity[Z] 0.59684E-29 c Pressure 0.37654E-03 11 0.24987E-07 0.54565E-01 0.13891E-02 c TempK 0.35847E+02 94 0.57563E-03 0.27667E-01 0.55074E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.26554 0.18992 2.9638e-005 2.9638e-005 v Velocity[Y] -0.28417 1.0225 0.011842 0.011842 v Velocity[Z] -5.2275e-014 5.0579e-014 -1.3169e-016 -1.3169e-016 v ǁVelocityǁ 0.00054083 1.0227 0.071061 0.071061 v Pressure -1.0061 1.0069 -4.1744e-016 1.6263e-016 v TempK 291.82 304.86 294.36 294.36 v Density 1 1 1 1 v CourantNb 0.3697 8 7.2824 7.2824 v FourierNb 0.14933 7.9996 0.78846 0.78846 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31874 22.768 1.7131 1.7131 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.75 304.81 294.39 294.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75721 15.245 8.0709 8.0709 INSTANT 0.760000000E+01 TIME STEP NUMBER 76 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.49039E-03 0.45410E-01 Friction velocity uk : 0.49039E-03 0.45410E-01 Dimensionless distance yplus : 0.16748E+00 0.15509E+02 Friction thermal sca. tstar : -0.15358E+02 0.14476E+01 Rough dim-less th. sca. tplus : 0.11891E+00 0.11011E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.88641E-04 114 0.33202E+00 0.37135E-02 0.76318E+00 c Velocity[X] 0.60332E-03 c Velocity[Y] 0.31101E-02 c Velocity[Z] 0.56744E-29 c Pressure 0.36400E-03 11 0.27909E-07 0.51770E-01 0.15878E-02 c TempK 0.36059E+02 94 0.51810E-03 0.24721E-01 0.52121E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1704 0.20376 -3.4341e-006 -3.4341e-006 v Velocity[Y] -0.26096 0.93923 0.011401 0.011401 v Velocity[Z] -5.0281e-014 5.4197e-014 -1.3491e-016 -1.3491e-016 v ǁVelocityǁ 0.00062584 0.93958 0.070449 0.070449 v Pressure -1.0058 1.0055 -1.1635e-015 -5.421e-016 v TempK 291.9 305.37 294.37 294.37 v Density 1 1 1 1 v CourantNb 0.17134 8 7.239 7.239 v FourierNb 0.12384 8.5467 0.79504 0.79504 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28595 24.325 1.7279 1.7279 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.82 304.86 294.41 294.4 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.44711 15.227 8.034 8.034 INSTANT 0.770000000E+01 TIME STEP NUMBER 77 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.29410E-03 0.45479E-01 Friction velocity uk : 0.29410E-03 0.45479E-01 Dimensionless distance yplus : 0.10044E+00 0.15532E+02 Friction thermal sca. tstar : -0.63841E+01 0.17224E+01 Rough dim-less th. sca. tplus : 0.71314E-01 0.11028E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.88494E-04 113 0.32127E+00 0.33933E-02 0.73418E+00 c Velocity[X] 0.54109E-03 c Velocity[Y] 0.28522E-02 c Velocity[Z] 0.52634E-29 c Pressure 0.34666E-03 10 0.24533E-07 0.47488E-01 0.14133E-02 c TempK 0.35987E+02 93 0.64004E-03 0.21174E-01 0.48403E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17209 0.18193 2.4021e-006 2.4021e-006 v Velocity[Y] -0.26644 0.91884 0.011491 0.011491 v Velocity[Z] -4.9704e-014 5.3563e-014 -1.1918e-016 -1.1918e-016 v ǁVelocityǁ 0.00046611 0.91985 0.070113 0.070113 v Pressure -1.0069 1.0084 -1.4477e-015 -8.4568e-016 v TempK 291.98 305.76 294.38 294.38 v Density 1 1 1 1 v CourantNb 0.30848 8 7.1968 7.1968 v FourierNb 0.13423 9.4014 0.80618 0.80618 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28652 26.757 1.7528 1.7528 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.9 305.37 294.42 294.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89603 14.484 8.003 8.003 INSTANT 0.780000000E+01 TIME STEP NUMBER 78 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32141E-03 0.44040E-01 Friction velocity uk : 0.32141E-03 0.44040E-01 Dimensionless distance yplus : 0.10977E+00 0.15041E+02 Friction thermal sca. tstar : -0.42603E+02 0.26132E+01 Rough dim-less th. sca. tplus : 0.77936E-01 0.10679E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81359E-04 114 0.28586E+00 0.32839E-02 0.69653E+00 c Velocity[X] 0.53341E-03 c Velocity[Y] 0.27505E-02 c Velocity[Z] 0.47014E-29 c Pressure 0.36827E-03 11 0.23927E-07 0.47491E-01 0.13604E-02 c TempK 0.35725E+02 92 0.45540E-03 0.19439E-01 0.46440E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18336 0.20749 -1.4875e-005 -1.4875e-005 v Velocity[Y] -0.2731 1.0253 0.01177 0.01177 v Velocity[Z] -5.5551e-014 5.6661e-014 -1.2208e-016 -1.2208e-016 v ǁVelocityǁ 0.00016591 1.0258 0.07027 0.07027 v Pressure -1.0062 1.0065 -1.8296e-015 -1.1709e-015 v TempK 292.01 305.79 294.4 294.4 v Density 1 1 1 1 v CourantNb 0.11772 8 7.1397 7.1397 v FourierNb 0.14408 10 0.82216 0.82216 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30754 28.461 1.7885 1.7885 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.98 305.76 294.44 294.43 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.39748 16.261 7.9618 7.9618 INSTANT 0.790000000E+01 TIME STEP NUMBER 79 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.67810E-03 0.45170E-01 Friction velocity uk : 0.67810E-03 0.45170E-01 Dimensionless distance yplus : 0.23159E+00 0.15427E+02 Friction thermal sca. tstar : -0.73609E+01 0.58458E+01 Rough dim-less th. sca. tplus : 0.16443E+00 0.10953E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87208E-04 113 0.31844E+00 0.32576E-02 0.69429E+00 c Velocity[X] 0.53268E-03 c Velocity[Y] 0.27250E-02 c Velocity[Z] 0.50501E-29 c Pressure 0.34797E-03 10 0.24817E-07 0.43311E-01 0.13613E-02 c TempK 0.35600E+02 91 0.54721E-03 0.19047E-01 0.46683E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1837 0.23244 1.6353e-005 1.6353e-005 v Velocity[Y] -0.2936 0.96873 0.011591 0.011591 v Velocity[Z] -5.5983e-014 5.478e-014 -1.1743e-016 -1.1743e-016 v ǁVelocityǁ 0.00030597 0.96956 0.069551 0.069551 v Pressure -1.0063 1.0065 -3.8192e-016 2.8189e-016 v TempK 291.98 305.9 294.42 294.42 v Density 1 1 1 1 v CourantNb 0.3405 8 7.1572 7.1572 v FourierNb 0.15814 10 0.84012 0.84012 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33756 28.461 1.8274 1.8274 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.01 305.79 294.45 294.44 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.8406 16.698 7.9973 7.9973 INSTANT 0.800000000E+01 TIME STEP NUMBER 80 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11574E-02 0.39339E-01 Friction velocity uk : 0.11574E-02 0.39339E-01 Dimensionless distance yplus : 0.39528E+00 0.13435E+02 Friction thermal sca. tstar : -0.85150E+01 0.62489E+01 Rough dim-less th. sca. tplus : 0.28064E+00 0.95389E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87594E-04 112 0.29366E+00 0.31119E-02 0.66849E+00 c Velocity[X] 0.55759E-03 c Velocity[Y] 0.25543E-02 c Velocity[Z] 0.47383E-29 c Pressure 0.35107E-03 11 0.19114E-07 0.40889E-01 0.12942E-02 c TempK 0.35454E+02 90 0.57876E-03 0.18358E-01 0.44980E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17428 0.22457 -6.624e-006 -6.624e-006 v Velocity[Y] -0.27765 1.0386 0.011545 0.011545 v Velocity[Z] -5.4679e-014 5.1534e-014 -1.2354e-016 -1.2354e-016 v ǁVelocityǁ 0.00029747 1.0387 0.069476 0.069476 v Pressure -1.0058 1.0069 -3.1086e-016 3.1442e-016 v TempK 291.87 305.74 294.43 294.43 v Density 1 1 1 1 v CourantNb 0.16172 8 7.1206 7.1206 v FourierNb 0.14569 9.161 0.86222 0.86222 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32449 26.073 1.873 1.873 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.98 305.9 294.47 294.46 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.46626 17.161 7.9828 7.9828 INSTANT 0.810000000E+01 TIME STEP NUMBER 81 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.59675E-03 0.44780E-01 Friction velocity uk : 0.59675E-03 0.44780E-01 Dimensionless distance yplus : 0.20381E+00 0.15294E+02 Friction thermal sca. tstar : -0.10816E+02 0.30168E+01 Rough dim-less th. sca. tplus : 0.14470E+00 0.10858E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91705E-04 111 0.31769E+00 0.31524E-02 0.68444E+00 c Velocity[X] 0.52098E-03 c Velocity[Y] 0.26315E-02 c Velocity[Z] 0.43650E-29 c Pressure 0.34850E-03 10 0.18179E-07 0.37642E-01 0.12669E-02 c TempK 0.35442E+02 89 0.64904E-03 0.18899E-01 0.45364E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15341 0.20493 -1.2552e-006 -1.2552e-006 v Velocity[Y] -0.28858 0.87879 0.01148 0.01148 v Velocity[Z] -5.6388e-014 4.8247e-014 -1.1212e-016 -1.1212e-016 v ǁVelocityǁ 0.00072412 0.88587 0.069551 0.069551 v Pressure -1.0055 1.0065 -1.1635e-015 -6.5052e-016 v TempK 291.69 305.62 294.45 294.45 v Density 1 1 1 1 v CourantNb 0.48475 8 7.1875 7.1875 v FourierNb 0.14244 10 0.88898 0.88898 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30404 28.461 1.9322 1.9322 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.87 305.74 294.49 294.48 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.98337 16.306 8.0764 8.0764 INSTANT 0.820000000E+01 TIME STEP NUMBER 82 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.97523E-03 0.43609E-01 Friction velocity uk : 0.97523E-03 0.43609E-01 Dimensionless distance yplus : 0.33307E+00 0.14894E+02 Friction thermal sca. tstar : -0.47523E+01 0.26936E+01 Rough dim-less th. sca. tplus : 0.23648E+00 0.10574E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89592E-04 112 0.30356E+00 0.32137E-02 0.68546E+00 c Velocity[X] 0.50350E-03 c Velocity[Y] 0.27102E-02 c Velocity[Z] 0.41007E-29 c Pressure 0.34842E-03 9 0.18190E-07 0.39735E-01 0.11935E-02 c TempK 0.35422E+02 89 0.63076E-03 0.22278E-01 0.47153E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19684 0.1807 -2.4567e-005 -2.4567e-005 v Velocity[Y] -0.27285 1.0527 0.011532 0.011532 v Velocity[Z] -4.9939e-014 5.035e-014 -1.1773e-016 -1.1773e-016 v ǁVelocityǁ 0.00077613 1.0532 0.069969 0.069969 v Pressure -1.0069 1.0054 -2.0073e-015 -1.3878e-015 v TempK 291.47 305.45 294.47 294.47 v Density 1 1 1 1 v CourantNb 0.28649 8 7.1791 7.1791 v FourierNb 0.11724 9.8408 0.90672 0.90672 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29386 22.801 1.9671 1.9671 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.69 305.62 294.51 294.5 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69821 16.834 8.0858 8.0858 INSTANT 0.830000000E+01 TIME STEP NUMBER 83 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13409E-02 0.47538E-01 Friction velocity uk : 0.13409E-02 0.47538E-01 Dimensionless distance yplus : 0.45795E+00 0.16236E+02 Friction thermal sca. tstar : -0.42081E+01 0.23129E+01 Rough dim-less th. sca. tplus : 0.32513E+00 0.11527E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.92961E-04 111 0.30837E+00 0.33468E-02 0.72042E+00 c Velocity[X] 0.51516E-03 c Velocity[Y] 0.28317E-02 c Velocity[Z] 0.45469E-29 c Pressure 0.34274E-03 11 0.20429E-07 0.42515E-01 0.12451E-02 c TempK 0.35533E+02 90 0.66048E-03 0.23864E-01 0.48092E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19119 0.21235 -1.1226e-005 -1.1226e-005 v Velocity[Y] -0.24481 0.94104 0.011343 0.011343 v Velocity[Z] -4.7272e-014 5.124e-014 -1.1047e-016 -1.1047e-016 v ǁVelocityǁ 0.00031135 0.9439 0.06978 0.06978 v Pressure -1.0074 1.0076 -3.5527e-016 2.6021e-016 v TempK 291.24 305.88 294.49 294.49 v Density 1 1 1 1 v CourantNb 0.34038 8 7.2431 7.2431 v FourierNb 0.11774 8.8123 0.8972 0.8972 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30302 25.081 1.9442 1.9442 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.47 305.45 294.53 294.52 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.92133 16.566 8.1403 8.1403 INSTANT 0.840000000E+01 TIME STEP NUMBER 84 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10435E-02 0.44263E-01 Friction velocity uk : 0.10435E-02 0.44263E-01 Dimensionless distance yplus : 0.35640E+00 0.15117E+02 Friction thermal sca. tstar : -0.13618E+02 0.69266E+01 Rough dim-less th. sca. tplus : 0.25304E+00 0.10733E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85019E-04 112 0.29604E+00 0.29587E-02 0.65480E+00 c Velocity[X] 0.48615E-03 c Velocity[Y] 0.24726E-02 c Velocity[Z] 0.37701E-29 c Pressure 0.34602E-03 13 0.21770E-07 0.44464E-01 0.13107E-02 c TempK 0.35301E+02 93 0.63590E-03 0.25724E-01 0.50222E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1759 0.21287 -1.0544e-005 -1.0544e-005 v Velocity[Y] -0.27348 0.99227 0.011555 0.011555 v Velocity[Z] -5.3785e-014 4.8412e-014 -1.182e-016 -1.182e-016 v ǁVelocityǁ 0.00046938 0.99238 0.070639 0.070639 v Pressure -1.0058 1.0052 -1.3323e-015 -7.0473e-016 v TempK 291.04 306.18 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.061108 8 7.2535 7.2535 v FourierNb 0.12951 9.6936 0.88032 0.88032 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30838 27.589 1.9086 1.9086 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.24 305.88 294.54 294.53 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.50919 15.507 8.1338 8.1338 INSTANT 0.850000000E+01 TIME STEP NUMBER 85 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.65198E-03 0.45885E-01 Friction velocity uk : 0.65198E-03 0.45885E-01 Dimensionless distance yplus : 0.22267E+00 0.15671E+02 Friction thermal sca. tstar : -0.55486E+01 0.35253E+01 Rough dim-less th. sca. tplus : 0.15809E+00 0.11126E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.88954E-04 115 0.28445E+00 0.30012E-02 0.65568E+00 c Velocity[X] 0.50499E-03 c Velocity[Y] 0.24962E-02 c Velocity[Z] 0.44428E-29 c Pressure 0.34479E-03 10 0.21952E-07 0.45219E-01 0.11971E-02 c TempK 0.35129E+02 95 0.61455E-03 0.24374E-01 0.49379E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18277 0.19577 -8.5399e-007 -8.5399e-007 v Velocity[Y] -0.29344 0.99117 0.011441 0.011441 v Velocity[Z] -6.0475e-014 4.9699e-014 -1.1891e-016 -1.1891e-016 v ǁVelocityǁ 0.00034035 0.99294 0.071227 0.071227 v Pressure -1.005 1.0052 -7.1054e-016 -5.421e-017 v TempK 290.89 306.19 294.51 294.51 v Density 1 1 1 1 v CourantNb 0.57697 8 7.3868 7.3868 v FourierNb 0.13737 9.4008 0.85302 0.85302 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29323 24.192 1.8504 1.8504 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.04 306.18 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0864 17.401 8.2398 8.2398 INSTANT 0.860000000E+01 TIME STEP NUMBER 86 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.47655E-03 0.43042E-01 Friction velocity uk : 0.47655E-03 0.43042E-01 Dimensionless distance yplus : 0.16275E+00 0.14700E+02 Friction thermal sca. tstar : -0.61358E+01 0.21847E+01 Rough dim-less th. sca. tplus : 0.11555E+00 0.10437E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85679E-04 116 0.28352E+00 0.30499E-02 0.65950E+00 c Velocity[X] 0.50042E-03 c Velocity[Y] 0.25495E-02 c Velocity[Z] 0.46916E-29 c Pressure 0.34355E-03 10 0.28459E-07 0.52784E-01 0.11238E-02 c TempK 0.35300E+02 95 0.58205E-03 0.20636E-01 0.45230E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16707 0.20654 -1.5041e-005 -1.5041e-005 v Velocity[Y] -0.26752 0.98457 0.011469 0.011469 v Velocity[Z] -6.3708e-014 5.3712e-014 -1.2102e-016 -1.2102e-016 v ǁVelocityǁ 0.00098535 0.98535 0.071708 0.071708 v Pressure -1.0046 1.0056 -1.9629e-015 -1.3553e-015 v TempK 290.85 305.83 294.51 294.51 v Density 1 1 1 1 v CourantNb 0.44106 8 7.4467 7.4467 v FourierNb 0.14747 7.2827 0.80193 0.80193 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31821 15.545 1.7378 1.7378 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.89 306.19 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89406 14.799 8.2486 8.2486 INSTANT 0.870000000E+01 TIME STEP NUMBER 87 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.96348E-03 0.42217E-01 Friction velocity uk : 0.96348E-03 0.42217E-01 Dimensionless distance yplus : 0.32906E+00 0.14419E+02 Friction thermal sca. tstar : -0.72031E+01 0.17761E+01 Rough dim-less th. sca. tplus : 0.23363E+00 0.10237E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85859E-04 115 0.27933E+00 0.29475E-02 0.63843E+00 c Velocity[X] 0.52314E-03 c Velocity[Y] 0.24244E-02 c Velocity[Z] 0.49309E-29 c Pressure 0.34937E-03 11 0.26837E-07 0.60496E-01 0.10986E-02 c TempK 0.35359E+02 93 0.57545E-03 0.21572E-01 0.46374E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1532 0.21948 3.3323e-006 3.3323e-006 v Velocity[Y] -0.32794 0.90947 0.011538 0.011538 v Velocity[Z] -5.8937e-014 5.5428e-014 -1.1673e-016 -1.1673e-016 v ǁVelocityǁ 0.00017168 0.91066 0.072405 0.072405 v Pressure -1.0053 1.0067 -8.5265e-016 -2.9273e-016 v TempK 290.96 305.38 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.50579 8 7.4468 7.4468 v FourierNb 0.1536 5.5583 0.76569 0.76569 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32787 11.865 1.6591 1.6591 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.85 305.83 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.123 13.558 8.2125 8.2125 INSTANT 0.880000000E+01 TIME STEP NUMBER 88 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.52176E-03 0.42943E-01 Friction velocity uk : 0.52176E-03 0.42943E-01 Dimensionless distance yplus : 0.17820E+00 0.14666E+02 Friction thermal sca. tstar : -0.12698E+02 0.14276E+01 Rough dim-less th. sca. tplus : 0.12652E+00 0.10413E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87087E-04 115 0.28141E+00 0.29651E-02 0.64013E+00 c Velocity[X] 0.52582E-03 c Velocity[Y] 0.24393E-02 c Velocity[Z] 0.43080E-29 c Pressure 0.33828E-03 11 0.27847E-07 0.57890E-01 0.11109E-02 c TempK 0.35507E+02 91 0.56371E-03 0.20829E-01 0.46794E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17706 0.20976 -3.1021e-006 -3.1021e-006 v Velocity[Y] -0.35656 0.89505 0.01149 0.01149 v Velocity[Z] -6.0124e-014 5.3742e-014 -1.1176e-016 -1.1176e-016 v ǁVelocityǁ 0.00019412 0.89543 0.073016 0.073016 v Pressure -1.0057 1.0064 -1.7764e-017 5.9631e-016 v TempK 291.18 305.16 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.57957 8 7.482 7.482 v FourierNb 0.14087 5.7074 0.75008 0.75008 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30069 12.183 1.6264 1.6264 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.96 305.38 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1096 13.536 8.232 8.232 INSTANT 0.890000000E+01 TIME STEP NUMBER 89 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.70320E-04 0.44584E-01 Friction velocity uk : 0.70320E-04 0.44584E-01 Dimensionless distance yplus : 0.24016E-01 0.15227E+02 Friction thermal sca. tstar : -0.11178E+03 0.11755E+01 Rough dim-less th. sca. tplus : 0.17051E-01 0.10811E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87399E-04 115 0.26835E+00 0.30672E-02 0.65681E+00 c Velocity[X] 0.49725E-03 c Velocity[Y] 0.25700E-02 c Velocity[Z] 0.43146E-29 c Pressure 0.33215E-03 11 0.27558E-07 0.57604E-01 0.11027E-02 c TempK 0.35726E+02 91 0.56743E-03 0.23645E-01 0.48670E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18721 0.19061 5.1299e-006 5.1299e-006 v Velocity[Y] -0.32735 0.90686 0.011559 0.011559 v Velocity[Z] -5.89e-014 5.0762e-014 -1.209e-016 -1.209e-016 v ǁVelocityǁ 0.00077341 0.90791 0.073421 0.073421 v Pressure -1.0063 1.0069 -6.1284e-016 -9.7578e-017 v TempK 291.42 305.03 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.03199 8 7.4888 7.4888 v FourierNb 0.13747 6.2781 0.73642 0.73642 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29345 13.401 1.5977 1.5977 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.18 305.16 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.61694 12.837 8.2252 8.2252 INSTANT 0.900000000E+01 TIME STEP NUMBER 90 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.61211E-03 0.40632E-01 Friction velocity uk : 0.61211E-03 0.40632E-01 Dimensionless distance yplus : 0.20905E+00 0.13877E+02 Friction thermal sca. tstar : -0.39113E+02 0.10254E+01 Rough dim-less th. sca. tplus : 0.14843E+00 0.98525E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85994E-04 114 0.26471E+00 0.29879E-02 0.62765E+00 c Velocity[X] 0.51137E-03 c Velocity[Y] 0.24765E-02 c Velocity[Z] 0.38463E-29 c Pressure 0.34424E-03 11 0.30851E-07 0.59300E-01 0.11522E-02 c TempK 0.35805E+02 91 0.53815E-03 0.23376E-01 0.48766E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18648 0.18084 -1.6509e-005 -1.6509e-005 v Velocity[Y] -0.25421 0.9665 0.011684 0.011684 v Velocity[Z] -5.8537e-014 4.8131e-014 -1.2623e-016 -1.2623e-016 v ǁVelocityǁ 0.00063883 0.9677 0.073901 0.073901 v Pressure -1.0071 1.0068 -1.1458e-015 -5.8547e-016 v TempK 291.62 304.92 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.13472 8 7.4609 7.4609 v FourierNb 0.13677 6.9059 0.73052 0.73052 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29194 14.741 1.5853 1.5853 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.42 305.03 294.54 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.379 13.289 8.1914 8.1914 INSTANT 0.910000000E+01 TIME STEP NUMBER 91 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12021E-02 0.43019E-01 Friction velocity uk : 0.12021E-02 0.43019E-01 Dimensionless distance yplus : 0.41056E+00 0.14692E+02 Friction thermal sca. tstar : -0.35822E+01 0.96973E+00 Rough dim-less th. sca. tplus : 0.29149E+00 0.10431E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85939E-04 114 0.26864E+00 0.30960E-02 0.64282E+00 c Velocity[X] 0.53246E-03 c Velocity[Y] 0.25636E-02 c Velocity[Z] 0.41774E-29 c Pressure 0.33693E-03 11 0.29111E-07 0.55316E-01 0.11546E-02 c TempK 0.35879E+02 91 0.71266E-03 0.25250E-01 0.50697E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19296 0.19189 -1.7533e-006 -1.7533e-006 v Velocity[Y] -0.2524 0.89241 0.011578 0.011578 v Velocity[Z] -5.81e-014 6.1095e-014 -1.287e-016 -1.287e-016 v ǁVelocityǁ 0.00029366 0.89463 0.074529 0.074529 v Pressure -1.0071 1.0079 -1.9895e-015 -1.3878e-015 v TempK 291.74 304.95 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.30704 8 7.4477 7.4477 v FourierNb 0.13518 7.5965 0.72859 0.72859 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28855 16.215 1.5799 1.5799 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.62 304.92 294.54 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89601 13.434 8.1763 8.1763 INSTANT 0.920000000E+01 TIME STEP NUMBER 92 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.22831E-03 0.42088E-01 Friction velocity uk : 0.22831E-03 0.42088E-01 Dimensionless distance yplus : 0.77976E-01 0.14374E+02 Friction thermal sca. tstar : -0.23026E+02 0.94838E+00 Rough dim-less th. sca. tplus : 0.55362E-01 0.10205E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85839E-04 114 0.26522E+00 0.32252E-02 0.66935E+00 c Velocity[X] 0.53013E-03 c Velocity[Y] 0.26950E-02 c Velocity[Z] 0.47023E-29 c Pressure 0.32901E-03 11 0.21845E-07 0.51289E-01 0.11160E-02 c TempK 0.36046E+02 90 0.50737E-03 0.25729E-01 0.52105E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22003 0.17494 -4.347e-006 -4.347e-006 v Velocity[Y] -0.28754 0.95516 0.011697 0.011697 v Velocity[Z] -5.8165e-014 4.8614e-014 -1.1996e-016 -1.1996e-016 v ǁVelocityǁ 0.0006786 0.95557 0.074505 0.074505 v Pressure -1.0069 1.0079 -9.1482e-016 -3.7947e-016 v TempK 291.84 304.98 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.20115 8 7.4573 7.4573 v FourierNb 0.14385 8.3561 0.7276 0.7276 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31674 17.837 1.5775 1.5775 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.74 304.95 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57202 15.542 8.1849 8.1849 INSTANT 0.930000000E+01 TIME STEP NUMBER 93 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.92952E-03 0.43137E-01 Friction velocity uk : 0.92952E-03 0.43137E-01 Dimensionless distance yplus : 0.31746E+00 0.14733E+02 Friction thermal sca. tstar : -0.22848E+02 0.93860E+00 Rough dim-less th. sca. tplus : 0.22539E+00 0.10460E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89731E-04 113 0.27510E+00 0.32059E-02 0.66741E+00 c Velocity[X] 0.51903E-03 c Velocity[Y] 0.26868E-02 c Velocity[Z] 0.44479E-29 c Pressure 0.33859E-03 11 0.18691E-07 0.50618E-01 0.10959E-02 c TempK 0.36063E+02 90 0.48877E-03 0.22201E-01 0.48668E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21263 0.16798 8.0151e-006 8.0151e-006 v Velocity[Y] -0.3088 0.87362 0.011411 0.011411 v Velocity[Z] -5.7453e-014 4.7357e-014 -1.0611e-016 -1.0611e-016 v ǁVelocityǁ 0.0011395 0.87938 0.073991 0.073991 v Pressure -1.0069 1.0086 -2.8422e-016 2.3852e-016 v TempK 291.91 304.98 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.41686 8 7.4628 7.4628 v FourierNb 0.1428 9.1918 0.73079 0.73079 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30482 19.62 1.5838 1.5838 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.84 304.98 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.66631 16.748 8.1936 8.1936 INSTANT 0.940000000E+01 TIME STEP NUMBER 94 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12524E-02 0.41276E-01 Friction velocity uk : 0.12524E-02 0.41276E-01 Dimensionless distance yplus : 0.42772E+00 0.14097E+02 Friction thermal sca. tstar : -0.45204E+01 0.95165E+00 Rough dim-less th. sca. tplus : 0.30367E+00 0.10009E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87762E-04 114 0.28760E+00 0.30543E-02 0.65445E+00 c Velocity[X] 0.52568E-03 c Velocity[Y] 0.25286E-02 c Velocity[Z] 0.42999E-29 c Pressure 0.34579E-03 10 0.21943E-07 0.50548E-01 0.11832E-02 c TempK 0.36078E+02 90 0.53812E-03 0.20123E-01 0.47579E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18703 0.19099 -1.0735e-006 -1.0735e-006 v Velocity[Y] -0.32083 0.8692 0.011383 0.011383 v Velocity[Z] -5.4878e-014 4.811e-014 -1.1685e-016 -1.1685e-016 v ǁVelocityǁ 0.00058048 0.86934 0.074103 0.074103 v Pressure -1.0072 1.0072 -9.9476e-016 -3.4694e-016 v TempK 291.91 304.98 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.39861 8 7.4252 7.4252 v FourierNb 0.12091 9.618 0.73611 0.73611 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28762 20.53 1.5947 1.5947 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.91 304.98 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81668 16.347 8.1613 8.1613 INSTANT 0.950000000E+01 TIME STEP NUMBER 95 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10715E-02 0.44964E-01 Friction velocity uk : 0.10715E-02 0.44964E-01 Dimensionless distance yplus : 0.36597E+00 0.15357E+02 Friction thermal sca. tstar : -0.52334E+01 0.92025E+00 Rough dim-less th. sca. tplus : 0.25983E+00 0.10903E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87941E-04 114 0.28048E+00 0.30494E-02 0.65338E+00 c Velocity[X] 0.52751E-03 c Velocity[Y] 0.25219E-02 c Velocity[Z] 0.44562E-29 c Pressure 0.33419E-03 11 0.20736E-07 0.47651E-01 0.10254E-02 c TempK 0.36064E+02 89 0.62838E-03 0.19125E-01 0.46460E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20511 0.15138 2.934e-005 2.934e-005 v Velocity[Y] -0.29333 0.90109 0.011323 0.011323 v Velocity[Z] -5.1939e-014 4.9802e-014 -1.1243e-016 -1.1243e-016 v ǁVelocityǁ 0.00027383 0.9039 0.073944 0.073944 v Pressure -1.0073 1.0064 -1.7586e-015 -1.1384e-015 v TempK 291.78 304.89 294.49 294.49 v Density 1 1 1 1 v CourantNb 0.32976 8 7.4411 7.4411 v FourierNb 0.1321 10 0.74261 0.74261 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29197 21.346 1.6084 1.6084 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.91 304.98 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.98601 14.655 8.1837 8.1837 INSTANT 0.960000000E+01 TIME STEP NUMBER 96 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.17215E-02 0.42631E-01 Friction velocity uk : 0.17215E-02 0.42631E-01 Dimensionless distance yplus : 0.58796E+00 0.14560E+02 Friction thermal sca. tstar : -0.59369E+01 0.10908E+01 Rough dim-less th. sca. tplus : 0.41744E+00 0.10337E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.87286E-04 115 0.27823E+00 0.31032E-02 0.65489E+00 c Velocity[X] 0.51596E-03 c Velocity[Y] 0.25872E-02 c Velocity[Z] 0.44513E-29 c Pressure 0.33952E-03 11 0.22663E-07 0.48303E-01 0.11705E-02 c TempK 0.36144E+02 88 0.59936E-03 0.17441E-01 0.45063E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19738 0.17248 4.7926e-007 4.7926e-007 v Velocity[Y] -0.2921 0.85737 0.011435 0.011435 v Velocity[Z] -5.0307e-014 5.0846e-014 -1.1738e-016 -1.1738e-016 v ǁVelocityǁ 0.00069133 0.85895 0.074125 0.074125 v Pressure -1.0066 1.0087 -2.8422e-016 2.9273e-016 v TempK 291.56 304.76 294.49 294.49 v Density 1 1 1 1 v CourantNb 0.1452 8 7.4739 7.4739 v FourierNb 0.13841 10 0.74588 0.74588 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29544 21.346 1.6159 1.6159 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.78 304.89 294.54 294.53 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.42488 17.114 8.2198 8.2198 INSTANT 0.970000000E+01 TIME STEP NUMBER 97 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.55828E-03 0.44644E-01 Friction velocity uk : 0.55828E-03 0.44644E-01 Dimensionless distance yplus : 0.19067E+00 0.15247E+02 Friction thermal sca. tstar : -0.13295E+02 0.14794E+01 Rough dim-less th. sca. tplus : 0.13537E+00 0.10825E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.86234E-04 115 0.27737E+00 0.29091E-02 0.63177E+00 c Velocity[X] 0.50709E-03 c Velocity[Y] 0.24020E-02 c Velocity[Z] 0.47610E-29 c Pressure 0.34181E-03 11 0.28272E-07 0.53069E-01 0.14095E-02 c TempK 0.36243E+02 87 0.66025E-03 0.17783E-01 0.44599E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16831 0.1532 2.472e-005 2.472e-005 v Velocity[Y] -0.26858 0.91166 0.011406 0.011406 v Velocity[Z] -5.0098e-014 5.1598e-014 -1.1285e-016 -1.1285e-016 v ǁVelocityǁ 0.00065 0.91271 0.073945 0.073945 v Pressure -1.0055 1.0071 -8.793e-016 -3.0358e-016 v TempK 291.37 305.22 294.48 294.48 v Density 1 1 1 1 v CourantNb 0.4223 8 7.4856 7.4856 v FourierNb 0.13583 8.818 0.74169 0.74169 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28994 18.822 1.6073 1.6073 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.56 304.76 294.54 294.53 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.98071 16.818 8.2273 8.2273 INSTANT 0.980000000E+01 TIME STEP NUMBER 98 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.45835E-03 0.42210E-01 Friction velocity uk : 0.45835E-03 0.42210E-01 Dimensionless distance yplus : 0.15654E+00 0.14416E+02 Friction thermal sca. tstar : -0.54399E+01 0.37048E+01 Rough dim-less th. sca. tplus : 0.11114E+00 0.10235E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81440E-04 116 0.27102E+00 0.28377E-02 0.60021E+00 c Velocity[X] 0.49516E-03 c Velocity[Y] 0.23426E-02 c Velocity[Z] 0.46730E-29 c Pressure 0.35007E-03 11 0.25042E-07 0.52262E-01 0.12284E-02 c TempK 0.36164E+02 86 0.59542E-03 0.14650E-01 0.41743E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16433 0.19005 9.4867e-006 9.4867e-006 v Velocity[Y] -0.26909 0.95492 0.011785 0.011785 v Velocity[Z] -5.4129e-014 5.3235e-014 -1.0193e-016 -1.0193e-016 v ǁVelocityǁ 0.00034108 0.95506 0.074195 0.074195 v Pressure -1.005 1.0075 -2.3981e-016 3.9031e-016 v TempK 291.3 305.4 294.48 294.48 v Density 1 1 1 1 v CourantNb 0.28943 8 7.463 7.463 v FourierNb 0.14941 9.6997 0.73737 0.73737 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31894 20.705 1.5978 1.5978 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.37 305.22 294.54 294.53 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.56412 17.543 8.2004 8.2004 INSTANT 0.990000000E+01 TIME STEP NUMBER 99 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12523E-02 0.44307E-01 Friction velocity uk : 0.12523E-02 0.44307E-01 Dimensionless distance yplus : 0.42770E+00 0.15132E+02 Friction thermal sca. tstar : -0.13698E+02 0.16306E+01 Rough dim-less th. sca. tplus : 0.30366E+00 0.10744E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83124E-04 116 0.29210E+00 0.33121E-02 0.67546E+00 c Velocity[X] 0.54972E-03 c Velocity[Y] 0.27624E-02 c Velocity[Z] 0.45654E-29 c Pressure 0.34109E-03 13 0.24978E-07 0.53633E-01 0.12854E-02 c TempK 0.36049E+02 86 0.69781E-03 0.15891E-01 0.41862E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18669 0.16013 1.5882e-005 1.5882e-005 v Velocity[Y] -0.26975 1.0349 0.0116 0.0116 v Velocity[Z] -5.8588e-014 5.4359e-014 -1.2896e-016 -1.2896e-016 v ǁVelocityǁ 0.00033097 1.0357 0.073936 0.073936 v Pressure -1.0047 1.0076 -2.6645e-016 3.6863e-016 v TempK 291.32 305.03 294.49 294.49 v Density 1 1 1 1 v CourantNb 0.25704 8 7.4622 7.4622 v FourierNb 0.16436 6.4673 0.73278 0.73278 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35083 13.805 1.5883 1.5883 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.3 305.4 294.54 294.53 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.68392 13.51 8.1949 8.1949 INSTANT 0.100000000E+02 TIME STEP NUMBER 100 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.63476E-03 0.41910E-01 Friction velocity uk : 0.63476E-03 0.41910E-01 Dimensionless distance yplus : 0.21679E+00 0.14313E+02 Friction thermal sca. tstar : -0.36084E+01 0.10023E+01 Rough dim-less th. sca. tplus : 0.15392E+00 0.10162E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81271E-04 116 0.29980E+00 0.31026E-02 0.65319E+00 c Velocity[X] 0.48829E-03 c Velocity[Y] 0.26143E-02 c Velocity[Z] 0.48909E-29 c Pressure 0.34775E-03 11 0.25864E-07 0.55932E-01 0.12555E-02 c TempK 0.35915E+02 86 0.56890E-03 0.13072E-01 0.38957E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16945 0.15879 -7.3232e-006 -7.3232e-006 v Velocity[Y] -0.29056 0.82189 0.011605 0.011605 v Velocity[Z] -5.6173e-014 5.4682e-014 -1.4436e-016 -1.4436e-016 v ǁVelocityǁ 0.00059182 0.82199 0.073658 0.073658 v Pressure -1.0044 1.006 -1.0036e-015 -3.2526e-016 v TempK 291.35 304.92 294.5 294.5 v Density 1 1 1 1 v CourantNb 0.43899 8 7.4804 7.4804 v FourierNb 0.14891 6.2884 0.72724 0.72724 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31787 13.423 1.5764 1.5764 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.32 305.03 294.55 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.98376 13.963 8.2076 8.2076 INSTANT 0.101000000E+02 TIME STEP NUMBER 101 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.29267E-03 0.43285E-01 Friction velocity uk : 0.29267E-03 0.43285E-01 Dimensionless distance yplus : 0.99957E-01 0.14783E+02 Friction thermal sca. tstar : -0.97355E+01 0.41696E+01 Rough dim-less th. sca. tplus : 0.70968E-01 0.10496E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81338E-04 115 0.29431E+00 0.28222E-02 0.61501E+00 c Velocity[X] 0.46819E-03 c Velocity[Y] 0.23541E-02 c Velocity[Z] 0.45458E-29 c Pressure 0.34617E-03 11 0.28002E-07 0.59951E-01 0.11436E-02 c TempK 0.35716E+02 86 0.70610E-03 0.11766E-01 0.36784E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15853 0.16046 1.217e-005 1.217e-005 v Velocity[Y] -0.30495 0.85498 0.011732 0.011732 v Velocity[Z] -5.2639e-014 5.5159e-014 -1.1321e-016 -1.1321e-016 v ǁVelocityǁ 0.00044197 0.85503 0.073595 0.073595 v Pressure -1.0038 1.006 -2.558e-015 -1.9732e-015 v TempK 291.35 304.77 294.51 294.51 v Density 1 1 1 1 v CourantNb 0.41274 8 7.4722 7.4722 v FourierNb 0.14402 6.9173 0.72139 0.72139 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30741 14.765 1.5636 1.5636 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.35 304.92 294.56 294.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1721 13.762 8.1936 8.1936 INSTANT 0.102000000E+02 TIME STEP NUMBER 102 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10863E-02 0.42468E-01 Friction velocity uk : 0.10863E-02 0.42468E-01 Dimensionless distance yplus : 0.37101E+00 0.14504E+02 Friction thermal sca. tstar : -0.45472E+01 0.11464E+01 Rough dim-less th. sca. tplus : 0.26341E+00 0.10298E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83616E-04 115 0.30951E+00 0.30828E-02 0.65473E+00 c Velocity[X] 0.48193E-03 c Velocity[Y] 0.26008E-02 c Velocity[Z] 0.49030E-29 c Pressure 0.34032E-03 11 0.29323E-07 0.60006E-01 0.12113E-02 c TempK 0.35623E+02 86 0.60006E-03 0.11543E-01 0.36770E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17846 0.18284 9.6695e-007 9.6695e-007 v Velocity[Y] -0.26899 0.96394 0.011721 0.011721 v Velocity[Z] -5.5362e-014 5.5267e-014 -1.2412e-016 -1.2412e-016 v ǁVelocityǁ 0.001141 0.96533 0.073116 0.073116 v Pressure -1.0066 1.0067 -2.5757e-016 3.7947e-016 v TempK 291.28 304.66 294.52 294.52 v Density 1 1 1 1 v CourantNb 0.32861 8 7.4579 7.4579 v FourierNb 0.14231 7.609 0.71627 0.71627 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30377 16.242 1.5534 1.5534 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.35 304.77 294.57 294.56 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0732 15.511 8.1742 8.1742 INSTANT 0.103000000E+02 TIME STEP NUMBER 103 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.94636E-03 0.45736E-01 Friction velocity uk : 0.94636E-03 0.45736E-01 Dimensionless distance yplus : 0.32321E+00 0.15620E+02 Friction thermal sca. tstar : -0.64295E+01 0.22833E+01 Rough dim-less th. sca. tplus : 0.22947E+00 0.11090E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.84805E-04 116 0.30278E+00 0.31068E-02 0.66466E+00 c Velocity[X] 0.48764E-03 c Velocity[Y] 0.26191E-02 c Velocity[Z] 0.46711E-29 c Pressure 0.33802E-03 11 0.30553E-07 0.64232E-01 0.13162E-02 c TempK 0.35556E+02 86 0.71294E-03 0.10809E-01 0.34884E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17885 0.19742 8.6509e-006 8.6509e-006 v Velocity[Y] -0.29596 0.86208 0.011552 0.011552 v Velocity[Z] -6.1731e-014 6.3084e-014 -1.1063e-016 -1.1063e-016 v ǁVelocityǁ 0.00019958 0.8621 0.072393 0.072393 v Pressure -1.0089 1.0083 9.77e-017 6.5052e-016 v TempK 291.12 304.51 294.54 294.54 v Density 1 1 1 1 v CourantNb 0.44136 8 7.4378 7.4378 v FourierNb 0.12772 5.8628 0.71104 0.71104 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28548 14.759 1.5421 1.5421 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.28 304.66 294.58 294.57 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73451 13.863 8.1489 8.1489 INSTANT 0.104000000E+02 TIME STEP NUMBER 104 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.42285E-03 0.43339E-01 Friction velocity uk : 0.42285E-03 0.43339E-01 Dimensionless distance yplus : 0.14442E+00 0.14802E+02 Friction thermal sca. tstar : -0.10899E+02 0.14072E+01 Rough dim-less th. sca. tplus : 0.10253E+00 0.10509E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82909E-04 115 0.30732E+00 0.31327E-02 0.67024E+00 c Velocity[X] 0.46208E-03 c Velocity[Y] 0.26706E-02 c Velocity[Z] 0.43983E-29 c Pressure 0.33459E-03 11 0.32377E-07 0.64211E-01 0.13781E-02 c TempK 0.35399E+02 86 0.58083E-03 0.11267E-01 0.35394E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20588 0.22663 3.818e-006 3.818e-006 v Velocity[Y] -0.31956 1.0035 0.011496 0.011496 v Velocity[Z] -5.796e-014 5.5739e-014 -1.2104e-016 -1.2104e-016 v ǁVelocityǁ 0.00045181 1.0079 0.071733 0.071733 v Pressure -1.0085 1.0066 -5.1514e-016 1.0842e-016 v TempK 290.97 304.69 294.55 294.55 v Density 1 1 1 1 v CourantNb 0.1292 8 7.3985 7.3985 v FourierNb 0.12455 5.7044 0.71185 0.71185 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29322 16.235 1.5451 1.5451 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.12 304.51 294.6 294.58 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.71842 13.088 8.1103 8.1103 INSTANT 0.105000000E+02 TIME STEP NUMBER 105 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.40647E-03 0.44653E-01 Friction velocity uk : 0.40647E-03 0.44653E-01 Dimensionless distance yplus : 0.13882E+00 0.15250E+02 Friction thermal sca. tstar : -0.60507E+01 0.13770E+01 Rough dim-less th. sca. tplus : 0.98561E-01 0.10827E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.84648E-04 114 0.30061E+00 0.31143E-02 0.67525E+00 c Velocity[X] 0.48316E-03 c Velocity[Y] 0.26311E-02 c Velocity[Z] 0.45795E-29 c Pressure 0.34407E-03 11 0.29149E-07 0.65001E-01 0.12573E-02 c TempK 0.35199E+02 87 0.67187E-03 0.12273E-01 0.36491E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24601 0.16493 2.2778e-005 2.2778e-005 v Velocity[Y] -0.31893 0.85047 0.011531 0.011531 v Velocity[Z] -5.8903e-014 5.8737e-014 -1.1284e-016 -1.1284e-016 v ǁVelocityǁ 0.0011896 0.85221 0.071547 0.071547 v Pressure -1.007 1.0069 -6.839e-016 -2.06e-016 v TempK 290.93 304.75 294.56 294.56 v Density 1 1 1 1 v CourantNb 0.18363 8 7.3866 7.3866 v FourierNb 0.13701 5.5022 0.71584 0.71584 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31971 14.511 1.5542 1.5542 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.97 304.69 294.61 294.6 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89127 13.479 8.1024 8.1024 INSTANT 0.106000000E+02 TIME STEP NUMBER 106 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.60338E-03 0.39963E-01 Friction velocity uk : 0.60338E-03 0.39963E-01 Dimensionless distance yplus : 0.20607E+00 0.13649E+02 Friction thermal sca. tstar : -0.39402E+01 0.41937E+01 Rough dim-less th. sca. tplus : 0.14631E+00 0.96903E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82923E-04 114 0.30836E+00 0.31141E-02 0.66416E+00 c Velocity[X] 0.49171E-03 c Velocity[Y] 0.26223E-02 c Velocity[Z] 0.45048E-29 c Pressure 0.34501E-03 11 0.31832E-07 0.63635E-01 0.11980E-02 c TempK 0.35010E+02 87 0.55311E-03 0.12143E-01 0.35570E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16651 0.18807 -8.1574e-006 -8.1574e-006 v Velocity[Y] -0.26727 1.0205 0.011561 0.011561 v Velocity[Z] -6.0047e-014 5.9579e-014 -1.0443e-016 -1.0443e-016 v ǁVelocityǁ 0.00064943 1.021 0.070778 0.070778 v Pressure -1.0071 1.0075 -4.6185e-016 1.4095e-016 v TempK 291.01 304.94 294.58 294.58 v Density 1 1 1 1 v CourantNb 0.48891 8 7.4021 7.4021 v FourierNb 0.14326 6.0525 0.72161 0.72161 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30579 15.686 1.5679 1.5679 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 290.93 304.75 294.62 294.61 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.7293 13.511 8.1237 8.1237 INSTANT 0.107000000E+02 TIME STEP NUMBER 107 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.82166E-03 0.41956E-01 Friction velocity uk : 0.82166E-03 0.41956E-01 Dimensionless distance yplus : 0.28062E+00 0.14329E+02 Friction thermal sca. tstar : -0.20299E+02 0.14084E+01 Rough dim-less th. sca. tplus : 0.19924E+00 0.10173E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83074E-04 115 0.30471E+00 0.32253E-02 0.69401E+00 c Velocity[X] 0.49687E-03 c Velocity[Y] 0.27284E-02 c Velocity[Z] 0.51649E-29 c Pressure 0.33691E-03 11 0.34305E-07 0.62716E-01 0.12863E-02 c TempK 0.35020E+02 87 0.58793E-03 0.12694E-01 0.37059E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18678 0.19789 1.1826e-006 1.1826e-006 v Velocity[Y] -0.30881 0.85132 0.011506 0.011506 v Velocity[Z] -5.4141e-014 5.9718e-014 -1.2529e-016 -1.2529e-016 v ǁVelocityǁ 0.00019539 0.85473 0.069869 0.069869 v Pressure -1.0073 1.0078 -1.3323e-015 -6.5052e-016 v TempK 291.1 304.97 294.59 294.59 v Density 1 1 1 1 v CourantNb 0.37619 8 7.3559 7.3559 v FourierNb 0.12846 6.6577 0.72391 0.72391 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29119 14.211 1.5699 1.5699 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.01 304.94 294.63 294.62 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.87512 12.669 8.0798 8.0798 INSTANT 0.108000000E+02 TIME STEP NUMBER 108 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10075E-02 0.41016E-01 Friction velocity uk : 0.10075E-02 0.41016E-01 Dimensionless distance yplus : 0.34411E+00 0.14008E+02 Friction thermal sca. tstar : -0.44443E+01 0.72507E+01 Rough dim-less th. sca. tplus : 0.24431E+00 0.99456E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79920E-04 115 0.30013E+00 0.29636E-02 0.65877E+00 c Velocity[X] 0.46534E-03 c Velocity[Y] 0.24982E-02 c Velocity[Z] 0.45368E-29 c Pressure 0.34244E-03 11 0.31596E-07 0.60954E-01 0.13682E-02 c TempK 0.34810E+02 88 0.50769E-03 0.13001E-01 0.37214E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20534 0.19936 -1.6232e-005 -1.6232e-005 v Velocity[Y] -0.33591 0.9919 0.0118 0.0118 v Velocity[Z] -5.0885e-014 5.8612e-014 -1.2683e-016 -1.2683e-016 v ǁVelocityǁ 0.00085396 0.99194 0.069355 0.069355 v Pressure -1.0087 1.0081 -2.0695e-015 -1.5613e-015 v TempK 291.17 305.14 294.6 294.6 v Density 1 1 1 1 v CourantNb 0.44102 8 7.3169 7.3169 v FourierNb 0.14131 7.3235 0.72753 0.72753 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31096 15.632 1.5778 1.5778 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.1 304.97 294.65 294.63 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.90413 13.905 8.0444 8.0444 INSTANT 0.109000000E+02 TIME STEP NUMBER 109 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.88420E-03 0.41358E-01 Friction velocity uk : 0.88420E-03 0.41358E-01 Dimensionless distance yplus : 0.30198E+00 0.14125E+02 Friction thermal sca. tstar : -0.44252E+01 0.14854E+01 Rough dim-less th. sca. tplus : 0.21440E+00 0.10028E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80053E-04 115 0.29430E+00 0.28637E-02 0.63211E+00 c Velocity[X] 0.45953E-03 c Velocity[Y] 0.24042E-02 c Velocity[Z] 0.47653E-29 c Pressure 0.35143E-03 11 0.31215E-07 0.62634E-01 0.12266E-02 c TempK 0.34457E+02 88 0.54029E-03 0.11619E-01 0.34689E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22658 0.19071 -2.1202e-006 -2.1202e-006 v Velocity[Y] -0.35232 1.1205 0.011905 0.011905 v Velocity[Z] -4.7387e-014 5.6918e-014 -1.1995e-016 -1.1995e-016 v ǁVelocityǁ 0.001499 1.1208 0.069168 0.069168 v Pressure -1.0107 1.0058 1.5099e-016 7.481e-016 v TempK 291.28 304.89 294.61 294.61 v Density 1 1 1 1 v CourantNb 0.34989 8 7.2776 7.2776 v FourierNb 0.15047 6.4627 0.73458 0.73458 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32118 13.795 1.5939 1.5939 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.17 305.14 294.66 294.65 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.8351 14.463 8.0122 8.0122 INSTANT 0.110000000E+02 TIME STEP NUMBER 110 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.46643E-03 0.41541E-01 Friction velocity uk : 0.46643E-03 0.41541E-01 Dimensionless distance yplus : 0.15930E+00 0.14187E+02 Friction thermal sca. tstar : -0.90268E+01 0.18528E+01 Rough dim-less th. sca. tplus : 0.11310E+00 0.10073E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81634E-04 115 0.29803E+00 0.29101E-02 0.63920E+00 c Velocity[X] 0.46239E-03 c Velocity[Y] 0.24477E-02 c Velocity[Z] 0.49251E-29 c Pressure 0.34936E-03 10 0.30210E-07 0.61125E-01 0.12198E-02 c TempK 0.34329E+02 88 0.43841E-03 0.12267E-01 0.36275E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24321 0.19512 -7.9576e-006 -7.9576e-006 v Velocity[Y] -0.33309 0.96768 0.011805 0.011805 v Velocity[Z] -5.0091e-014 5.5991e-014 -1.1315e-016 -1.1315e-016 v ǁVelocityǁ 0.00031478 0.96776 0.068648 0.068648 v Pressure -1.0116 1.0072 -7.9048e-016 -1.9516e-016 v TempK 291.51 305.09 294.62 294.62 v Density 1 1 1 1 v CourantNb 0.32758 8 7.2331 7.2331 v FourierNb 0.13947 5.9875 0.74454 0.74454 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32286 14.507 1.6166 1.6166 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.28 304.89 294.67 294.66 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75464 13.597 7.9777 7.9777 INSTANT 0.111000000E+02 TIME STEP NUMBER 111 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.77225E-03 0.41576E-01 Friction velocity uk : 0.77225E-03 0.41576E-01 Dimensionless distance yplus : 0.26375E+00 0.14200E+02 Friction thermal sca. tstar : -0.65739E+01 0.75656E+01 Rough dim-less th. sca. tplus : 0.18726E+00 0.10081E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.84611E-04 115 0.29673E+00 0.27813E-02 0.62107E+00 c Velocity[X] 0.47993E-03 c Velocity[Y] 0.23014E-02 c Velocity[Z] 0.50669E-29 c Pressure 0.34833E-03 10 0.33188E-07 0.59801E-01 0.13073E-02 c TempK 0.34173E+02 87 0.57645E-03 0.12321E-01 0.35643E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.25285 0.25756 1.3263e-007 1.3263e-007 v Velocity[Y] -0.42928 0.96851 0.011773 0.011773 v Velocity[Z] -5.4137e-014 5.5178e-014 -1.0573e-016 -1.0573e-016 v ǁVelocityǁ 0.00017319 0.9686 0.068646 0.068646 v Pressure -1.0114 1.0076 -3.2863e-016 3.0358e-016 v TempK 291.84 305.02 294.64 294.64 v Density 1 1 1 1 v CourantNb 0.49654 8 7.1831 7.1831 v FourierNb 0.13938 6.4782 0.75798 0.75798 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29752 15.957 1.6467 1.6467 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.51 305.09 294.68 294.67 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81222 14.478 7.941 7.941 INSTANT 0.112000000E+02 TIME STEP NUMBER 112 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.60439E-03 0.42226E-01 Friction velocity uk : 0.60439E-03 0.42226E-01 Dimensionless distance yplus : 0.20642E+00 0.14422E+02 Friction thermal sca. tstar : -0.19122E+02 0.39443E+01 Rough dim-less th. sca. tplus : 0.14655E+00 0.10239E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 112, Physical time 0.11200E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: 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 0.87159E-04 115 0.29568E+00 0.27994E-02 0.62195E+00 c Velocity[X] 0.43392E-03 c Velocity[Y] 0.23655E-02 c Velocity[Z] 0.59289E-29 c Pressure 0.33504E-03 11 0.35215E-07 0.59835E-01 0.12554E-02 c TempK 0.34245E+02 87 0.45569E-03 0.12142E-01 0.37470E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24981 0.24628 -3.1609e-005 -3.1609e-005 v Velocity[Y] -0.47288 0.94845 0.011868 0.011868 v Velocity[Z] -5.454e-014 5.244e-014 -1.1637e-016 -1.1637e-016 v ǁVelocityǁ 0.00019517 0.94856 0.068623 0.068623 v Pressure -1.0105 1.0052 -3.4639e-016 3.1442e-016 v TempK 292.16 304.74 294.66 294.66 v Density 1 1 1 1 v CourantNb 0.16602 8 7.1482 7.1482 v FourierNb 0.13212 6.1674 0.76607 0.76607 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28289 17.553 1.6657 1.6657 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.84 305.02 294.7 294.69 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1322 12.014 7.9143 7.9143 INSTANT 0.113000000E+02 TIME STEP NUMBER 113 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.65224E-03 0.41828E-01 Friction velocity uk : 0.65224E-03 0.41828E-01 Dimensionless distance yplus : 0.22276E+00 0.14285E+02 Friction thermal sca. tstar : -0.52801E+01 0.40123E+01 Rough dim-less th. sca. tplus : 0.15816E+00 0.10142E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.88494E-04 115 0.29721E+00 0.27845E-02 0.61000E+00 c Velocity[X] 0.41124E-03 c Velocity[Y] 0.23732E-02 c Velocity[Z] 0.52056E-29 c Pressure 0.35241E-03 11 0.37860E-07 0.61087E-01 0.12303E-02 c TempK 0.34356E+02 88 0.58820E-03 0.11604E-01 0.36641E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23209 0.19528 -1.4729e-005 -1.4729e-005 v Velocity[Y] -0.49941 0.87413 0.011965 0.011965 v Velocity[Z] -5.1703e-014 5.0305e-014 -9.6359e-017 -9.6359e-017 v ǁVelocityǁ 0.00062154 0.8772 0.068719 0.068719 v Pressure -1.0105 1.0041 -2.0783e-015 -1.4854e-015 v TempK 292.34 304.56 294.68 294.68 v Density 1 1 1 1 v CourantNb 0.22277 8 7.0829 7.0829 v FourierNb 0.13375 6.7842 0.77789 0.77789 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28549 19.308 1.6928 1.6928 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.16 304.74 294.72 294.71 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.56151 13.097 7.8608 7.8608 INSTANT 0.114000000E+02 TIME STEP NUMBER 114 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.86135E-03 0.38731E-01 Friction velocity uk : 0.86135E-03 0.38731E-01 Dimensionless distance yplus : 0.29418E+00 0.13228E+02 Friction thermal sca. tstar : -0.43892E+01 0.17313E+01 Rough dim-less th. sca. tplus : 0.20886E+00 0.93915E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94009E-04 114 0.29168E+00 0.29158E-02 0.62715E+00 c Velocity[X] 0.44056E-03 c Velocity[Y] 0.24753E-02 c Velocity[Z] 0.55900E-29 c Pressure 0.36421E-03 11 0.36081E-07 0.61140E-01 0.12308E-02 c TempK 0.34469E+02 89 0.56553E-03 0.13078E-01 0.38841E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18363 0.18859 -3.2136e-005 -3.2136e-005 v Velocity[Y] -0.49615 0.89298 0.011969 0.011969 v Velocity[Z] -5.4699e-014 5.6447e-014 -1.1545e-016 -1.1545e-016 v ǁVelocityǁ 0.00050583 0.89358 0.068499 0.068499 v Pressure -1.0104 1.0046 -8.5265e-016 -3.2526e-016 v TempK 292.38 304.45 294.7 294.7 v Density 1 1 1 1 v CourantNb 0.28051 8 7.0931 7.0931 v FourierNb 0.13207 5.8206 0.78716 0.78716 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28192 16.484 1.7121 1.7121 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.34 304.56 294.74 294.73 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.54775 13.553 7.8803 7.8803 INSTANT 0.115000000E+02 TIME STEP NUMBER 115 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.51589E-03 0.46112E-01 Friction velocity uk : 0.51589E-03 0.46112E-01 Dimensionless distance yplus : 0.17619E+00 0.15749E+02 Friction thermal sca. tstar : -0.18714E+02 0.10902E+01 Rough dim-less th. sca. tplus : 0.12509E+00 0.11181E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10028E-03 114 0.29791E+00 0.30097E-02 0.65348E+00 c Velocity[X] 0.44300E-03 c Velocity[Y] 0.25667E-02 c Velocity[Z] 0.56496E-29 c Pressure 0.35310E-03 11 0.36267E-07 0.57492E-01 0.13477E-02 c TempK 0.34411E+02 91 0.66003E-03 0.17061E-01 0.43323E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16577 0.17916 -1.4785e-006 -1.4785e-006 v Velocity[Y] -0.50999 1.0354 0.011822 0.011822 v Velocity[Z] -4.6364e-014 5.4837e-014 -1.1246e-016 -1.1246e-016 v ǁVelocityǁ 0.00044483 1.0391 0.067995 0.067995 v Pressure -1.0108 1.0077 -8.9706e-016 -4.12e-016 v TempK 292.34 303.92 294.72 294.72 v Density 1 1 1 1 v CourantNb 0.42233 8 7.0743 7.0743 v FourierNb 0.12027 6.4026 0.79301 0.79301 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28258 14.607 1.7214 1.7214 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.38 304.45 294.76 294.74 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.8131 13.087 7.8674 7.8674 INSTANT 0.116000000E+02 TIME STEP NUMBER 116 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.56052E-03 0.42329E-01 Friction velocity uk : 0.56052E-03 0.42329E-01 Dimensionless distance yplus : 0.19144E+00 0.14457E+02 Friction thermal sca. tstar : -0.22654E+02 0.14032E+01 Rough dim-less th. sca. tplus : 0.13592E+00 0.10264E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97756E-04 115 0.29059E+00 0.32141E-02 0.69040E+00 c Velocity[X] 0.44496E-03 c Velocity[Y] 0.27691E-02 c Velocity[Z] 0.59583E-29 c Pressure 0.34348E-03 11 0.34773E-07 0.54185E-01 0.13156E-02 c TempK 0.34200E+02 92 0.53184E-03 0.20593E-01 0.48209E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14435 0.22692 -3.1406e-005 -3.1406e-005 v Velocity[Y] -0.51688 1.0327 0.011788 0.011788 v Velocity[Z] -4.8478e-014 5.66e-014 -1.2744e-016 -1.2744e-016 v ǁVelocityǁ 0.00035812 1.0362 0.067584 0.067584 v Pressure -1.0102 1.0065 -1.4744e-015 -7.9147e-016 v TempK 292.28 303.06 294.74 294.74 v Density 1 1 1 1 v CourantNb 0.19717 8 7.0501 7.0501 v FourierNb 0.11799 7.0429 0.79927 0.79927 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30823 15.49 1.7344 1.7344 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.34 303.92 294.78 294.77 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.46427 13.602 7.8494 7.8494 INSTANT 0.117000000E+02 TIME STEP NUMBER 117 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.72703E-03 0.43946E-01 Friction velocity uk : 0.72703E-03 0.43946E-01 Dimensionless distance yplus : 0.24830E+00 0.15009E+02 Friction thermal sca. tstar : -0.47277E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.17629E+00 0.10656E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94284E-04 115 0.28890E+00 0.30474E-02 0.66469E+00 c Velocity[X] 0.49589E-03 c Velocity[Y] 0.25515E-02 c Velocity[Z] 0.57999E-29 c Pressure 0.34628E-03 11 0.36017E-07 0.55494E-01 0.13359E-02 c TempK 0.34120E+02 93 0.53134E-03 0.22910E-01 0.50241E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.12843 0.26551 1.8191e-005 1.8191e-005 v Velocity[Y] -0.45694 1.0086 0.01169 0.01169 v Velocity[Z] -5.518e-014 6.0045e-014 -1.227e-016 -1.227e-016 v ǁVelocityǁ 0.00054354 1.0098 0.067095 0.067095 v Pressure -1.0086 1.007 9.3259e-016 1.5613e-015 v TempK 292.21 302.89 294.75 294.75 v Density 1 1 1 1 v CourantNb 0.27941 8 7.0558 7.0558 v FourierNb 0.12499 6.8018 0.7931 0.7931 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32412 15.807 1.721 1.721 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.28 303.15 294.8 294.78 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85865 13.657 7.8489 7.8489 INSTANT 0.118000000E+02 TIME STEP NUMBER 118 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12102E-02 0.46778E-01 Friction velocity uk : 0.12102E-02 0.46778E-01 Dimensionless distance yplus : 0.41333E+00 0.15976E+02 Friction thermal sca. tstar : -0.51426E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.29346E+00 0.11343E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91369E-04 115 0.28508E+00 0.27417E-02 0.62165E+00 c Velocity[X] 0.46096E-03 c Velocity[Y] 0.22807E-02 c Velocity[Z] 0.59253E-29 c Pressure 0.34433E-03 10 0.34297E-07 0.57324E-01 0.12276E-02 c TempK 0.33929E+02 92 0.50431E-03 0.23405E-01 0.49466E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14781 0.24423 6.2195e-006 6.2195e-006 v Velocity[Y] -0.37005 1.0608 0.011663 0.011663 v Velocity[Z] -6.713e-014 4.8964e-014 -1.29e-016 -1.29e-016 v ǁVelocityǁ 0.00043969 1.061 0.066891 0.066891 v Pressure -1.0074 1.005 -3.4639e-016 1.7347e-016 v TempK 292.13 302.92 294.76 294.76 v Density 1 1 1 1 v CourantNb 0.24205 8 7.0636 7.0636 v FourierNb 0.13473 5.8364 0.79167 0.79167 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30406 16.611 1.7186 1.7186 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.21 303.15 294.81 294.8 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.46965 13.836 7.8553 7.8553 INSTANT 0.119000000E+02 TIME STEP NUMBER 119 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11090E-02 0.44310E-01 Friction velocity uk : 0.11090E-02 0.44310E-01 Dimensionless distance yplus : 0.37877E+00 0.15133E+02 Friction thermal sca. tstar : -0.39453E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.26892E+00 0.10744E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91711E-04 116 0.29035E+00 0.29117E-02 0.65687E+00 c Velocity[X] 0.43376E-03 c Velocity[Y] 0.24780E-02 c Velocity[Z] 0.54987E-29 c Pressure 0.33665E-03 11 0.32498E-07 0.58011E-01 0.11724E-02 c TempK 0.33774E+02 92 0.51221E-03 0.22283E-01 0.47236E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18166 0.19122 1.4747e-005 1.4747e-005 v Velocity[Y] -0.40643 1.1398 0.011857 0.011857 v Velocity[Z] -7.2824e-014 5.315e-014 -1.328e-016 -1.328e-016 v ǁVelocityǁ 0.000645 1.1403 0.067131 0.067131 v Pressure -1.0071 1.0085 1.0125e-015 1.648e-015 v TempK 291.99 302.92 294.77 294.77 v Density 1 1 1 1 v CourantNb 0.22786 8 7.0963 7.0963 v FourierNb 0.14821 5.7596 0.78932 0.78932 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32072 16.392 1.7141 1.7141 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.13 303.15 294.82 294.81 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85419 12.488 7.8856 7.8856 INSTANT 0.120000000E+02 TIME STEP NUMBER 120 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.69262E-03 0.45714E-01 Friction velocity uk : 0.69262E-03 0.45714E-01 Dimensionless distance yplus : 0.23655E+00 0.15613E+02 Friction thermal sca. tstar : -0.11502E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.16795E+00 0.11085E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89644E-04 115 0.29875E+00 0.27485E-02 0.61449E+00 c Velocity[X] 0.45298E-03 c Velocity[Y] 0.22955E-02 c Velocity[Z] 0.50530E-29 c Pressure 0.35377E-03 11 0.35468E-07 0.64348E-01 0.11879E-02 c TempK 0.33446E+02 93 0.49595E-03 0.21546E-01 0.46328E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17887 0.22863 2.2025e-006 2.2025e-006 v Velocity[Y] -0.40835 1.0493 0.012055 0.012055 v Velocity[Z] -7.4568e-014 5.0352e-014 -1.2711e-016 -1.2711e-016 v ǁVelocityǁ 0.00047961 1.0497 0.067136 0.067136 v Pressure -1.0059 1.0062 -9.5035e-016 -2.6021e-016 v TempK 291.8 302.76 294.78 294.78 v Density 1 1 1 1 v CourantNb 0.52608 8 7.1523 7.1523 v FourierNb 0.13918 4.7758 0.78958 0.78958 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29709 13.592 1.7141 1.7141 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.99 303.15 294.83 294.82 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.98967 12.776 7.9419 7.9419 INSTANT 0.121000000E+02 TIME STEP NUMBER 121 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14929E-03 0.43119E-01 Friction velocity uk : 0.14929E-03 0.43119E-01 Dimensionless distance yplus : 0.50987E-01 0.14726E+02 Friction thermal sca. tstar : -0.19200E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.36200E-01 0.10456E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91929E-04 115 0.31216E+00 0.29527E-02 0.63960E+00 c Velocity[X] 0.47694E-03 c Velocity[Y] 0.24758E-02 c Velocity[Z] 0.49893E-29 c Pressure 0.34258E-03 11 0.31342E-07 0.63273E-01 0.11816E-02 c TempK 0.33266E+02 94 0.62850E-03 0.20598E-01 0.44060E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19152 0.27799 1.7392e-005 1.7392e-005 v Velocity[Y] -0.346 1.0428 0.011996 0.011996 v Velocity[Z] -7.5279e-014 5.1028e-014 -1.2009e-016 -1.2009e-016 v ǁVelocityǁ 0.00025778 1.0437 0.067899 0.067899 v Pressure -1.0062 1.0077 2.0428e-016 8.1315e-016 v TempK 291.62 302.76 294.79 294.79 v Density 1 1 1 1 v CourantNb 0.28814 8 7.1752 7.1752 v FourierNb 0.11978 3.7711 0.79168 0.79168 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30438 10.651 1.7184 1.7184 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.8 303.15 294.84 294.83 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1061 11.771 7.9669 7.9669 INSTANT 0.122000000E+02 TIME STEP NUMBER 122 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.76847E-03 0.44734E-01 Friction velocity uk : 0.76847E-03 0.44734E-01 Dimensionless distance yplus : 0.26246E+00 0.15278E+02 Friction thermal sca. tstar : -0.90212E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.18634E+00 0.10847E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91741E-04 115 0.31251E+00 0.30933E-02 0.67273E+00 c Velocity[X] 0.48701E-03 c Velocity[Y] 0.26063E-02 c Velocity[Z] 0.45963E-29 c Pressure 0.34609E-03 11 0.32347E-07 0.66837E-01 0.12250E-02 c TempK 0.33514E+02 94 0.51512E-03 0.19774E-01 0.43837E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17188 0.24892 -4.2303e-006 -4.2303e-006 v Velocity[Y] -0.33043 0.97852 0.011632 0.011632 v Velocity[Z] -6.7366e-014 4.8136e-014 -1.3798e-016 -1.3798e-016 v ǁVelocityǁ 0.00048676 0.97855 0.068155 0.068155 v Pressure -1.0072 1.006 -1.0125e-015 -4.2284e-016 v TempK 291.51 302.92 294.79 294.79 v Density 1 1 1 1 v CourantNb 0.16172 8 7.2814 7.2814 v FourierNb 0.12479 3.8582 0.78504 0.78504 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30119 9.765 1.7044 1.7044 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.62 303.15 294.85 294.83 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.63139 11.858 8.0665 8.0665 INSTANT 0.123000000E+02 TIME STEP NUMBER 123 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32109E-03 0.45553E-01 Friction velocity uk : 0.32109E-03 0.45553E-01 Dimensionless distance yplus : 0.10966E+00 0.15558E+02 Friction thermal sca. tstar : -0.26935E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.77857E-01 0.11046E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.88864E-04 117 0.30485E+00 0.27154E-02 0.62354E+00 c Velocity[X] 0.44808E-03 c Velocity[Y] 0.22673E-02 c Velocity[Z] 0.49901E-29 c Pressure 0.34392E-03 11 0.32761E-07 0.66217E-01 0.13332E-02 c TempK 0.33621E+02 93 0.53535E-03 0.18184E-01 0.41929E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17047 0.23872 1.9325e-005 1.9325e-005 v Velocity[Y] -0.29832 1.0957 0.011623 0.011623 v Velocity[Z] -7.4532e-014 5.1101e-014 -9.5263e-017 -9.5263e-017 v ǁVelocityǁ 0.00034015 1.0972 0.068442 0.068442 v Pressure -1.005 1.0074 -1.0036e-015 -4.12e-016 v TempK 291.46 303.13 294.79 294.79 v Density 1 1 1 1 v CourantNb 0.22502 8 7.3182 7.3182 v FourierNb 0.13727 4.2126 0.77405 0.77405 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30671 10.742 1.6814 1.6814 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.51 303.15 294.85 294.84 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.51954 11.829 8.0923 8.0923 INSTANT 0.124000000E+02 TIME STEP NUMBER 124 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12633E-02 0.45052E-01 Friction velocity uk : 0.12633E-02 0.45052E-01 Dimensionless distance yplus : 0.43144E+00 0.15387E+02 Friction thermal sca. tstar : -0.47805E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.30632E+00 0.10924E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.86643E-04 117 0.30387E+00 0.26860E-02 0.60836E+00 c Velocity[X] 0.44245E-03 c Velocity[Y] 0.22435E-02 c Velocity[Z] 0.43813E-29 c Pressure 0.35842E-03 11 0.32443E-07 0.69866E-01 0.12961E-02 c TempK 0.33645E+02 91 0.53404E-03 0.16647E-01 0.40843E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19318 0.2028 6.368e-006 6.368e-006 v Velocity[Y] -0.26441 0.945 0.011797 0.011797 v Velocity[Z] -6.4179e-014 5.1213e-014 -1.2439e-016 -1.2439e-016 v ǁVelocityǁ 0.00072405 0.94501 0.069177 0.069177 v Pressure -1.0048 1.0066 -4.4409e-017 6.0715e-016 v TempK 291.47 303.28 294.8 294.8 v Density 1 1 1 1 v CourantNb 0.30577 8 7.324 7.324 v FourierNb 0.14197 4.6338 0.76 0.76 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30304 11.805 1.6506 1.6506 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.46 303.15 294.85 294.84 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.62383 11.921 8.084 8.084 INSTANT 0.125000000E+02 TIME STEP NUMBER 125 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.89024E-03 0.47602E-01 Friction velocity uk : 0.89024E-03 0.47602E-01 Dimensionless distance yplus : 0.30405E+00 0.16258E+02 Friction thermal sca. tstar : -0.14842E+02 0.22109E+00 Rough dim-less th. sca. tplus : 0.21587E+00 0.11543E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83828E-04 117 0.31077E+00 0.29834E-02 0.65180E+00 c Velocity[X] 0.50452E-03 c Velocity[Y] 0.24789E-02 c Velocity[Z] 0.40705E-29 c Pressure 0.35977E-03 11 0.33968E-07 0.71499E-01 0.12277E-02 c TempK 0.33612E+02 89 0.65895E-03 0.17093E-01 0.41484E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19045 0.19508 1.5123e-005 1.5123e-005 v Velocity[Y] -0.25756 0.98391 0.01176 0.01176 v Velocity[Z] -6.76e-014 5.1476e-014 -1.0152e-016 -1.0152e-016 v ǁVelocityǁ 0.00076955 0.98459 0.069018 0.069018 v Pressure -1.0045 1.0079 -3.1974e-016 2.6021e-016 v TempK 291.49 303.2 294.81 294.81 v Density 1 1 1 1 v CourantNb 0.42888 8 7.347 7.347 v FourierNb 0.14035 5.0972 0.74702 0.74702 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2996 12.986 1.6212 1.6212 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.47 303.28 294.86 294.85 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.98543 11.946 8.094 8.094 INSTANT 0.126000000E+02 TIME STEP NUMBER 126 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.80223E-03 0.44471E-01 Friction velocity uk : 0.80223E-03 0.44471E-01 Dimensionless distance yplus : 0.27399E+00 0.15188E+02 Friction thermal sca. tstar : -0.80441E+01 0.64966E-01 Rough dim-less th. sca. tplus : 0.19453E+00 0.10783E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83282E-04 117 0.31551E+00 0.29714E-02 0.65633E+00 c Velocity[X] 0.48694E-03 c Velocity[Y] 0.24845E-02 c Velocity[Z] 0.42537E-29 c Pressure 0.34604E-03 11 0.33625E-07 0.70008E-01 0.12997E-02 c TempK 0.33600E+02 89 0.66720E-03 0.18866E-01 0.43376E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1517 0.19463 -4.2819e-006 -4.2819e-006 v Velocity[Y] -0.26813 0.97908 0.011728 0.011728 v Velocity[Z] -6.1237e-014 5.481e-014 -1.1157e-016 -1.1157e-016 v ǁVelocityǁ 0.0018481 0.97925 0.069253 0.069253 v Pressure -1.005 1.0078 -8.8818e-018 5.421e-016 v TempK 291.44 303.16 294.81 294.81 v Density 1 1 1 1 v CourantNb 0.30753 8 7.3562 7.3562 v FourierNb 0.12273 5.3688 0.74436 0.74436 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26197 14.284 1.615 1.615 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.49 303.2 294.87 294.85 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89961 13.369 8.1006 8.1006 INSTANT 0.127000000E+02 TIME STEP NUMBER 127 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10829E-02 0.46678E-01 Friction velocity uk : 0.10829E-02 0.46678E-01 Dimensionless distance yplus : 0.36985E+00 0.15942E+02 Friction thermal sca. tstar : -0.81164E+01 0.14077E-01 Rough dim-less th. sca. tplus : 0.26259E+00 0.11319E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82502E-04 116 0.33077E+00 0.29567E-02 0.65813E+00 c Velocity[X] 0.47636E-03 c Velocity[Y] 0.24804E-02 c Velocity[Z] 0.46139E-29 c Pressure 0.35516E-03 13 0.31112E-07 0.71287E-01 0.14453E-02 c TempK 0.33694E+02 89 0.61768E-03 0.20145E-01 0.45344E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16473 0.21761 1.4849e-005 1.4849e-005 v Velocity[Y] -0.29981 0.98199 0.011728 0.011728 v Velocity[Z] -7.0927e-014 5.2657e-014 -9.605e-017 -9.605e-017 v ǁVelocityǁ 0.00095726 0.98216 0.068971 0.068971 v Pressure -1.0062 1.0078 3.7303e-016 8.9989e-016 v TempK 291.35 303.24 294.82 294.82 v Density 1 1 1 1 v CourantNb 0.3501 8 7.3892 7.3892 v FourierNb 0.12675 5.9057 0.74255 0.74255 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27056 15.713 1.6095 1.6095 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.44 303.16 294.87 294.86 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.861 12.414 8.1317 8.1317 INSTANT 0.128000000E+02 TIME STEP NUMBER 128 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10492E-02 0.44210E-01 Friction velocity uk : 0.10492E-02 0.44210E-01 Dimensionless distance yplus : 0.35834E+00 0.15099E+02 Friction thermal sca. tstar : -0.34571E+01 0.16668E+00 Rough dim-less th. sca. tplus : 0.25441E+00 0.10720E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85248E-04 115 0.32123E+00 0.31159E-02 0.69911E+00 c Velocity[X] 0.50220E-03 c Velocity[Y] 0.26137E-02 c Velocity[Z] 0.45254E-29 c Pressure 0.35228E-03 15 0.33601E-07 0.74995E-01 0.13909E-02 c TempK 0.33897E+02 88 0.63303E-03 0.17934E-01 0.44933E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18269 0.2339 5.1763e-006 5.1763e-006 v Velocity[Y] -0.33206 0.95974 0.011707 0.011707 v Velocity[Z] -5.9965e-014 5.5556e-014 -1.2303e-016 -1.2303e-016 v ǁVelocityǁ 0.0004117 0.95989 0.068622 0.068622 v Pressure -1.007 1.0071 -1.1102e-015 -5.6379e-016 v TempK 291.32 303.37 294.83 294.83 v Density 1 1 1 1 v CourantNb 0.29187 8 7.3697 7.3697 v FourierNb 0.13872 5.1699 0.73877 0.73877 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2961 14.714 1.6004 1.6004 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.35 303.24 294.88 294.87 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.61544 12.617 8.1084 8.1084 INSTANT 0.129000000E+02 TIME STEP NUMBER 129 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.66688E-03 0.47468E-01 Friction velocity uk : 0.66688E-03 0.47468E-01 Dimensionless distance yplus : 0.22776E+00 0.16212E+02 Friction thermal sca. tstar : -0.46698E+01 0.21754E+00 Rough dim-less th. sca. tplus : 0.16171E+00 0.11510E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.85238E-04 115 0.29443E+00 0.30799E-02 0.66519E+00 c Velocity[X] 0.50996E-03 c Velocity[Y] 0.25699E-02 c Velocity[Z] 0.39578E-29 c Pressure 0.34890E-03 11 0.35167E-07 0.75373E-01 0.14189E-02 c TempK 0.33931E+02 89 0.66580E-03 0.19490E-01 0.46456E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18276 0.2473 1.518e-005 1.518e-005 v Velocity[Y] -0.27916 0.98016 0.011848 0.011848 v Velocity[Z] -5.6931e-014 5.5931e-014 -1.2017e-016 -1.2017e-016 v ǁVelocityǁ 0.0011497 0.98068 0.069381 0.069381 v Pressure -1.0071 1.0074 -9.5923e-016 -4.12e-016 v TempK 291.4 303.58 294.85 294.85 v Density 1 1 1 1 v CourantNb 0.38567 8 7.3269 7.3269 v FourierNb 0.1311 4.7719 0.74172 0.74172 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27985 13.581 1.606 1.606 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.32 303.37 294.89 294.88 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60126 12.772 8.0686 8.0686 INSTANT 0.130000000E+02 TIME STEP NUMBER 130 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11372E-03 0.45888E-01 Friction velocity uk : 0.11372E-03 0.45888E-01 Dimensionless distance yplus : 0.38837E-01 0.15672E+02 Friction thermal sca. tstar : -0.64880E+01 0.70579E+00 Rough dim-less th. sca. tplus : 0.27574E-01 0.11127E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.90610E-04 116 0.29166E+00 0.35162E-02 0.73964E+00 c Velocity[X] 0.59326E-03 c Velocity[Y] 0.29229E-02 c Velocity[Z] 0.41307E-29 c Pressure 0.35173E-03 11 0.39298E-07 0.77599E-01 0.15011E-02 c TempK 0.34244E+02 90 0.63112E-03 0.19464E-01 0.45431E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18761 0.232 -1.7128e-006 -1.7128e-006 v Velocity[Y] -0.29388 0.94184 0.011485 0.011485 v Velocity[Z] -5.4003e-014 5.8784e-014 -1.3533e-016 -1.3533e-016 v ǁVelocityǁ 0.00075645 0.94194 0.069496 0.069496 v Pressure -1.0056 1.0093 -1.199e-015 -6.18e-016 v TempK 291.61 303.71 294.85 294.85 v Density 1 1 1 1 v CourantNb 0.50518 8 7.3917 7.3917 v FourierNb 0.12073 4.0119 0.74388 0.74388 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25771 11.418 1.6099 1.6099 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.4 303.58 294.9 294.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75751 12.012 8.1356 8.1356 INSTANT 0.131000000E+02 TIME STEP NUMBER 131 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10111E-02 0.43502E-01 Friction velocity uk : 0.10111E-02 0.43502E-01 Dimensionless distance yplus : 0.34531E+00 0.14857E+02 Friction thermal sca. tstar : -0.53714E+01 0.70270E+00 Rough dim-less th. sca. tplus : 0.24517E+00 0.10548E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.88763E-04 117 0.27248E+00 0.32825E-02 0.70467E+00 c Velocity[X] 0.57611E-03 c Velocity[Y] 0.27064E-02 c Velocity[Z] 0.44555E-29 c Pressure 0.34890E-03 11 0.36798E-07 0.78907E-01 0.13781E-02 c TempK 0.34431E+02 91 0.64326E-03 0.20471E-01 0.46379E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20693 0.24864 1.737e-005 1.737e-005 v Velocity[Y] -0.29089 0.96381 0.011355 0.011355 v Velocity[Z] -5.2306e-014 5.6014e-014 -1.1396e-016 -1.1396e-016 v ǁVelocityǁ 0.00026435 0.96392 0.06938 0.06938 v Pressure -1.0058 1.0079 -7.5495e-016 -2.3852e-016 v TempK 291.83 303.92 294.86 294.86 v Density 1 1 1 1 v CourantNb 0.18077 8 7.4113 7.4113 v FourierNb 0.12337 3.3715 0.74618 0.74618 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26334 9.5956 1.6147 1.6147 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.61 303.71 294.91 294.9 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.38008 11.371 8.1575 8.1575 INSTANT 0.132000000E+02 TIME STEP NUMBER 132 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14781E-02 0.46579E-01 Friction velocity uk : 0.14781E-02 0.46579E-01 Dimensionless distance yplus : 0.50482E+00 0.15908E+02 Friction thermal sca. tstar : -0.12023E+02 0.84825E+00 Rough dim-less th. sca. tplus : 0.35841E+00 0.11294E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.93655E-04 117 0.26171E+00 0.34341E-02 0.72360E+00 c Velocity[X] 0.60890E-03 c Velocity[Y] 0.28252E-02 c Velocity[Z] 0.40260E-29 c Pressure 0.36482E-03 11 0.37083E-07 0.85406E-01 0.12949E-02 c TempK 0.34759E+02 91 0.69832E-03 0.19776E-01 0.45349E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23463 0.21736 -4.3954e-006 -4.3954e-006 v Velocity[Y] -0.30665 0.92028 0.011138 0.011138 v Velocity[Z] -5.5482e-014 5.4842e-014 -1.3585e-016 -1.3585e-016 v ǁVelocityǁ 0.00033073 0.92056 0.069875 0.069875 v Pressure -1.0059 1.0087 -5.0626e-016 7.5894e-017 v TempK 291.95 304.04 294.87 294.87 v Density 1 1 1 1 v CourantNb 0.14085 8 7.4024 7.4024 v FourierNb 0.12415 3.1879 0.74759 0.74759 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.265 8.3731 1.6173 1.6173 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.83 303.92 294.92 294.91 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.93592 10.942 8.15 8.15 INSTANT 0.133000000E+02 TIME STEP NUMBER 133 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.64644E-03 0.43933E-01 Friction velocity uk : 0.64644E-03 0.43933E-01 Dimensionless distance yplus : 0.22078E+00 0.15004E+02 Friction thermal sca. tstar : -0.11360E+02 0.22686E+01 Rough dim-less th. sca. tplus : 0.15675E+00 0.10653E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94393E-04 117 0.25327E+00 0.33597E-02 0.72540E+00 c Velocity[X] 0.59525E-03 c Velocity[Y] 0.27645E-02 c Velocity[Z] 0.43335E-29 c Pressure 0.35692E-03 11 0.40075E-07 0.87068E-01 0.14048E-02 c TempK 0.35004E+02 90 0.71243E-03 0.22591E-01 0.49713E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.2441 0.19613 -4.9183e-006 -4.9183e-006 v Velocity[Y] -0.37707 0.84942 0.011102 0.011102 v Velocity[Z] -5.6941e-014 5.1172e-014 -1.3372e-016 -1.3372e-016 v ǁVelocityǁ 0.0015915 0.85366 0.069897 0.069897 v Pressure -1.0074 1.0089 -2.5757e-016 4.12e-016 v TempK 291.9 304.18 294.89 294.89 v Density 1 1 1 1 v CourantNb 0.43251 8 7.4156 7.4156 v FourierNb 0.12202 2.9579 0.74924 0.74924 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26047 6.3392 1.6206 1.6206 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.95 304.04 294.93 294.92 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85558 10.815 8.1648 8.1648 INSTANT 0.134000000E+02 TIME STEP NUMBER 134 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14736E-02 0.45764E-01 Friction velocity uk : 0.14736E-02 0.45764E-01 Dimensionless distance yplus : 0.50328E+00 0.15630E+02 Friction thermal sca. tstar : -0.50106E+01 0.12916E+01 Rough dim-less th. sca. tplus : 0.35732E+00 0.11097E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96439E-04 116 0.25047E+00 0.30420E-02 0.66891E+00 c Velocity[X] 0.53703E-03 c Velocity[Y] 0.25050E-02 c Velocity[Z] 0.44040E-29 c Pressure 0.33591E-03 11 0.39407E-07 0.81941E-01 0.14206E-02 c TempK 0.35200E+02 90 0.69688E-03 0.19570E-01 0.45563E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17887 0.17632 -2.7016e-005 -2.7016e-005 v Velocity[Y] -0.31825 0.94009 0.011373 0.011373 v Velocity[Z] -5.2445e-014 5.1434e-014 -1.2584e-016 -1.2584e-016 v ǁVelocityǁ 0.0010052 0.9401 0.070589 0.070589 v Pressure -1.0071 1.0071 -2.1316e-016 4.12e-016 v TempK 291.75 304.36 294.9 294.9 v Density 1 1 1 1 v CourantNb 0.44309 8 7.3922 7.3922 v FourierNb 0.11999 3.1839 0.75441 0.75441 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25612 6.9731 1.6307 1.6307 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.9 304.18 294.95 294.94 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.70394 11.099 8.1466 8.1466 INSTANT 0.135000000E+02 TIME STEP NUMBER 135 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.85619E-03 0.43564E-01 Friction velocity uk : 0.85619E-03 0.43564E-01 Dimensionless distance yplus : 0.29241E+00 0.14878E+02 Friction thermal sca. tstar : -0.18913E+02 0.10618E+01 Rough dim-less th. sca. tplus : 0.20761E+00 0.10563E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94992E-04 115 0.23686E+00 0.31711E-02 0.67242E+00 c Velocity[X] 0.57977E-03 c Velocity[Y] 0.25914E-02 c Velocity[Z] 0.48670E-29 c Pressure 0.35412E-03 11 0.38330E-07 0.87776E-01 0.13175E-02 c TempK 0.35355E+02 90 0.70796E-03 0.19670E-01 0.46432E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22707 0.18976 -1.2538e-005 -1.2538e-005 v Velocity[Y] -0.25395 0.89346 0.011329 0.011329 v Velocity[Z] -5.2564e-014 5.1062e-014 -1.19e-016 -1.19e-016 v ǁVelocityǁ 0.0023756 0.89364 0.070702 0.070702 v Pressure -1.0061 1.0067 0 5.6379e-016 v TempK 291.61 304.5 294.92 294.92 v Density 1 1 1 1 v CourantNb 0.088688 8 7.3878 7.3878 v FourierNb 0.13198 3.5023 0.75847 0.75847 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28173 7.6704 1.6397 1.6397 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.75 304.36 294.96 294.95 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57693 11.187 8.1462 8.1462 INSTANT 0.136000000E+02 TIME STEP NUMBER 136 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13079E-02 0.43581E-01 Friction velocity uk : 0.13079E-02 0.43581E-01 Dimensionless distance yplus : 0.44669E+00 0.14884E+02 Friction thermal sca. tstar : -0.56578E+01 0.12088E+01 Rough dim-less th. sca. tplus : 0.31714E+00 0.10568E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98397E-04 115 0.24305E+00 0.33469E-02 0.70392E+00 c Velocity[X] 0.61348E-03 c Velocity[Y] 0.27335E-02 c Velocity[Z] 0.42746E-29 c Pressure 0.34944E-03 11 0.43582E-07 0.87540E-01 0.13974E-02 c TempK 0.35702E+02 89 0.81993E-03 0.23512E-01 0.51057E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24365 0.18606 -2.7765e-005 -2.7765e-005 v Velocity[Y] -0.25918 1.0697 0.01112 0.01112 v Velocity[Z] -5.1988e-014 5.2191e-014 -1.2628e-016 -1.2628e-016 v ǁVelocityǁ 0.00029729 1.0747 0.071328 0.071328 v Pressure -1.0056 1.0092 -1.1546e-015 -4.5536e-016 v TempK 291.58 304.63 294.93 294.93 v Density 1 1 1 1 v CourantNb 0.45806 8 7.3896 7.3896 v FourierNb 0.14518 3.8525 0.76279 0.76279 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3099 8.2234 1.6493 1.6493 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.61 304.5 294.97 294.96 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85753 11.405 8.1524 8.1524 INSTANT 0.137000000E+02 TIME STEP NUMBER 137 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12757E-02 0.44792E-01 Friction velocity uk : 0.12757E-02 0.44792E-01 Dimensionless distance yplus : 0.43570E+00 0.15298E+02 Friction thermal sca. tstar : -0.44341E+01 0.20707E+01 Rough dim-less th. sca. tplus : 0.30934E+00 0.10861E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98393E-04 114 0.24828E+00 0.32701E-02 0.70000E+00 c Velocity[X] 0.53989E-03 c Velocity[Y] 0.27302E-02 c Velocity[Z] 0.50280E-29 c Pressure 0.34364E-03 11 0.42038E-07 0.85490E-01 0.14584E-02 c TempK 0.36072E+02 88 0.62537E-03 0.19376E-01 0.47705E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22265 0.18773 -1.2411e-005 -1.2411e-005 v Velocity[Y] -0.2555 0.92044 0.01127 0.01127 v Velocity[Z] -5.1968e-014 5.5101e-014 -1.262e-016 -1.262e-016 v ǁVelocityǁ 0.00094226 0.9264 0.07164 0.07164 v Pressure -1.0037 1.0079 -9.3259e-016 -3.5779e-016 v TempK 291.69 304.8 294.94 294.94 v Density 1 1 1 1 v CourantNb 0.11185 8 7.4452 7.4452 v FourierNb 0.1303 4.2377 0.76301 0.76301 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27813 9.0457 1.6495 1.6495 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.58 304.63 294.99 294.98 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.55923 11.96 8.2082 8.2082 INSTANT 0.138000000E+02 TIME STEP NUMBER 138 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.18281E-02 0.42705E-01 Friction velocity uk : 0.18281E-02 0.42705E-01 Dimensionless distance yplus : 0.62436E+00 0.14585E+02 Friction thermal sca. tstar : -0.31539E+01 0.22014E+01 Rough dim-less th. sca. tplus : 0.44328E+00 0.10355E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94461E-04 115 0.23047E+00 0.28777E-02 0.62125E+00 c Velocity[X] 0.55222E-03 c Velocity[Y] 0.23254E-02 c Velocity[Z] 0.42888E-29 c Pressure 0.37498E-03 12 0.39304E-07 0.91577E-01 0.13923E-02 c TempK 0.36128E+02 88 0.62341E-03 0.20230E-01 0.46570E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21904 0.18844 -2.8804e-005 -2.8804e-005 v Velocity[Y] -0.28629 0.87317 0.011649 0.011649 v Velocity[Z] -5.1387e-014 5.7262e-014 -1.3124e-016 -1.3124e-016 v ǁVelocityǁ 0.00062862 0.87481 0.072889 0.072889 v Pressure -1.0062 1.0093 -5.5067e-016 -1.0842e-017 v TempK 291.9 304.94 294.96 294.96 v Density 1 1 1 1 v CourantNb 0.27666 8 7.4101 7.4101 v FourierNb 0.13183 4.6615 0.76308 0.76308 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2814 9.9503 1.6497 1.6497 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.69 304.8 295 294.99 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.51274 11.974 8.1732 8.1732 INSTANT 0.139000000E+02 TIME STEP NUMBER 139 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.16506E-02 0.47170E-01 Friction velocity uk : 0.16506E-02 0.47170E-01 Dimensionless distance yplus : 0.56374E+00 0.16110E+02 Friction thermal sca. tstar : -0.32008E+01 0.23334E+01 Rough dim-less th. sca. tplus : 0.40025E+00 0.11438E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97871E-04 115 0.24926E+00 0.32765E-02 0.67544E+00 c Velocity[X] 0.63054E-03 c Velocity[Y] 0.26459E-02 c Velocity[Z] 0.46468E-29 c Pressure 0.37111E-03 11 0.39282E-07 0.86735E-01 0.14438E-02 c TempK 0.36493E+02 88 0.64099E-03 0.20599E-01 0.49018E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24834 0.19092 -1.1078e-005 -1.1078e-005 v Velocity[Y] -0.27487 0.91953 0.011436 0.011436 v Velocity[Z] -5.0581e-014 5.76e-014 -1.2313e-016 -1.2313e-016 v ǁVelocityǁ 0.00057445 0.93756 0.073354 0.073354 v Pressure -1.0068 1.008 -7.5495e-016 -4.3368e-017 v TempK 292.09 305.17 294.97 294.97 v Density 1 1 1 1 v CourantNb 0.32837 8 7.4591 7.4591 v FourierNb 0.13635 5.1277 0.76062 0.76062 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29105 10.945 1.6439 1.6439 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 291.9 304.94 295.01 295 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75452 12.328 8.2197 8.2197 INSTANT 0.140000000E+02 TIME STEP NUMBER 140 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.58274E-03 0.43533E-01 Friction velocity uk : 0.58274E-03 0.43533E-01 Dimensionless distance yplus : 0.19902E+00 0.14868E+02 Friction thermal sca. tstar : -0.41073E+01 0.15616E+01 Rough dim-less th. sca. tplus : 0.14130E+00 0.10556E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98263E-04 115 0.25078E+00 0.32599E-02 0.70416E+00 c Velocity[X] 0.58982E-03 c Velocity[Y] 0.26701E-02 c Velocity[Z] 0.48526E-29 c Pressure 0.36360E-03 12 0.38497E-07 0.81782E-01 0.15607E-02 c TempK 0.36810E+02 88 0.70999E-03 0.21175E-01 0.48829E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22027 0.18663 -9.0796e-006 -9.0796e-006 v Velocity[Y] -0.30566 0.86331 0.01121 0.01121 v Velocity[Z] -5.2664e-014 5.6069e-014 -1.0892e-016 -1.0892e-016 v ǁVelocityǁ 0.00057629 0.86333 0.073237 0.073237 v Pressure -1.0062 1.014 -6.2172e-016 3.2526e-017 v TempK 292.2 305.42 294.98 294.98 v Density 1 1 1 1 v CourantNb 0.18926 8 7.4853 7.4853 v FourierNb 0.13662 5.5981 0.75889 0.75889 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29163 11.95 1.64 1.64 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.09 305.17 295.03 295.01 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.43678 13.065 8.2442 8.2442 INSTANT 0.141000000E+02 TIME STEP NUMBER 141 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.30317E-03 0.49684E-01 Friction velocity uk : 0.30317E-03 0.49684E-01 Dimensionless distance yplus : 0.10354E+00 0.16969E+02 Friction thermal sca. tstar : -0.60703E+01 0.15278E+01 Rough dim-less th. sca. tplus : 0.73512E-01 0.12047E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96779E-04 114 0.25460E+00 0.27528E-02 0.61236E+00 c Velocity[X] 0.49655E-03 c Velocity[Y] 0.22562E-02 c Velocity[Z] 0.43344E-29 c Pressure 0.35498E-03 11 0.36493E-07 0.80357E-01 0.14426E-02 c TempK 0.36862E+02 88 0.56904E-03 0.19031E-01 0.46781E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21904 0.19539 -1.74e-005 -1.74e-005 v Velocity[Y] -0.30432 0.88532 0.011349 0.011349 v Velocity[Z] -5.732e-014 5.4339e-014 -1.1559e-016 -1.1559e-016 v ǁVelocityǁ 0.0010745 0.88626 0.073781 0.073781 v Pressure -1.0061 1.0082 -1.0481e-015 -4.5536e-016 v TempK 292.22 305.63 295 295 v Density 1 1 1 1 v CourantNb 0.31498 8 7.4618 7.4618 v FourierNb 0.12919 5.2942 0.75491 0.75491 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27576 11.301 1.6325 1.6325 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.2 305.42 295.04 295.03 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.62342 12.985 8.2167 8.2167 INSTANT 0.142000000E+02 TIME STEP NUMBER 142 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10633E-02 0.43680E-01 Friction velocity uk : 0.10633E-02 0.43680E-01 Dimensionless distance yplus : 0.36315E+00 0.14918E+02 Friction thermal sca. tstar : -0.36993E+01 0.28680E+01 Rough dim-less th. sca. tplus : 0.25783E+00 0.10592E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94162E-04 113 0.24959E+00 0.29682E-02 0.61808E+00 c Velocity[X] 0.54371E-03 c Velocity[Y] 0.24245E-02 c Velocity[Z] 0.45386E-29 c Pressure 0.36553E-03 11 0.34903E-07 0.80807E-01 0.13969E-02 c TempK 0.36849E+02 101 0.64790E-03 0.19641E-01 0.45763E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23794 0.18977 -2.1851e-005 -2.1851e-005 v Velocity[Y] -0.24896 0.84032 0.011393 0.011393 v Velocity[Z] -5.7729e-014 5.1533e-014 -1.1489e-016 -1.1489e-016 v ǁVelocityǁ 0.00061625 0.8412 0.074693 0.074693 v Pressure -1.0054 1.0087 -7.7272e-016 -2.06e-016 v TempK 292.23 305.91 295.01 295.01 v Density 1 1 1 1 v CourantNb 0.41497 8 7.4816 7.4816 v FourierNb 0.14099 5.1016 0.75213 0.75213 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30334 10.895 1.6262 1.6262 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.22 305.63 295.05 295.04 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.77823 12.665 8.2337 8.2337 INSTANT 0.143000000E+02 TIME STEP NUMBER 143 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.64128E-03 0.45910E-01 Friction velocity uk : 0.64128E-03 0.45910E-01 Dimensionless distance yplus : 0.21902E+00 0.15680E+02 Friction thermal sca. tstar : -0.58572E+01 0.14332E+01 Rough dim-less th. sca. tplus : 0.15550E+00 0.11132E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.93126E-04 115 0.25497E+00 0.32173E-02 0.67285E+00 c Velocity[X] 0.54270E-03 c Velocity[Y] 0.26746E-02 c Velocity[Z] 0.52643E-29 c Pressure 0.34451E-03 11 0.38500E-07 0.77623E-01 0.13133E-02 c TempK 0.37259E+02 88 0.64500E-03 0.19310E-01 0.45012E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23315 0.19106 3.2508e-006 3.2508e-006 v Velocity[Y] -0.25041 1.0666 0.011362 0.011362 v Velocity[Z] -5.313e-014 5.5731e-014 -1.1047e-016 -1.1047e-016 v ǁVelocityǁ 0.00086937 1.0667 0.074821 0.074821 v Pressure -1.0062 1.0072 -6.5725e-016 -5.421e-017 v TempK 292.3 306.09 295.03 295.03 v Density 1 1 1 1 v CourantNb 0.1693 8 7.5213 7.5213 v FourierNb 0.11051 4.7272 0.73985 0.73985 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2831 11.49 1.6003 1.6003 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.23 305.91 295.07 295.06 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89266 12.037 8.2612 8.2612 INSTANT 0.144000000E+02 TIME STEP NUMBER 144 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.99148E-03 0.43065E-01 Friction velocity uk : 0.99148E-03 0.43065E-01 Dimensionless distance yplus : 0.33862E+00 0.14708E+02 Friction thermal sca. tstar : -0.11674E+02 0.34160E+01 Rough dim-less th. sca. tplus : 0.24041E+00 0.10442E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91546E-04 114 0.28221E+00 0.30630E-02 0.64895E+00 c Velocity[X] 0.48167E-03 c Velocity[Y] 0.25813E-02 c Velocity[Z] 0.48768E-29 c Pressure 0.34979E-03 11 0.36835E-07 0.79245E-01 0.12110E-02 c TempK 0.37472E+02 88 0.63809E-03 0.16893E-01 0.43718E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19561 0.2045 -1.0818e-005 -1.0818e-005 v Velocity[Y] -0.2651 0.86175 0.011728 0.011728 v Velocity[Z] -5.4373e-014 5.0883e-014 -1.1183e-016 -1.1183e-016 v ǁVelocityǁ 0.00092882 0.87003 0.075097 0.075097 v Pressure -1.0073 1.0088 -5.4179e-016 7.5894e-017 v TempK 292.43 306.32 295.04 295.04 v Density 1 1 1 1 v CourantNb 0.42866 8 7.506 7.506 v FourierNb 0.12156 5.1999 0.72739 0.72739 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29657 11.1 1.5741 1.5741 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.3 306.09 295.08 295.07 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.71767 12.778 8.2334 8.2334 INSTANT 0.145000000E+02 TIME STEP NUMBER 145 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.17691E-02 0.43408E-01 Friction velocity uk : 0.17691E-02 0.43408E-01 Dimensionless distance yplus : 0.60421E+00 0.14825E+02 Friction thermal sca. tstar : -0.86123E+01 0.15699E+01 Rough dim-less th. sca. tplus : 0.42898E+00 0.10526E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91543E-04 114 0.27689E+00 0.29246E-02 0.62504E+00 c Velocity[X] 0.49929E-03 c Velocity[Y] 0.24253E-02 c Velocity[Z] 0.42828E-29 c Pressure 0.36781E-03 11 0.38405E-07 0.83113E-01 0.12387E-02 c TempK 0.37722E+02 88 0.67165E-03 0.17967E-01 0.44554E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19312 0.22241 -1.0121e-005 -1.0121e-005 v Velocity[Y] -0.29402 1.0409 0.01185 0.01185 v Velocity[Z] -5.1841e-014 6.0791e-014 -1.3106e-016 -1.3106e-016 v ǁVelocityǁ 0.0015526 1.041 0.075407 0.075407 v Pressure -1.0068 1.0069 -4.0856e-016 2.1684e-016 v TempK 292.55 306.16 295.05 295.05 v Density 1 1 1 1 v CourantNb 0.23867 8 7.5007 7.5007 v FourierNb 0.12709 4.8024 0.71702 0.71702 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27128 10.251 1.5524 1.5524 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.43 306.32 295.09 295.08 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.56625 12.635 8.2177 8.2177 INSTANT 0.146000000E+02 TIME STEP NUMBER 146 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10142E-02 0.42678E-01 Friction velocity uk : 0.10142E-02 0.42678E-01 Dimensionless distance yplus : 0.34637E+00 0.14576E+02 Friction thermal sca. tstar : -0.48180E+01 0.60900E+01 Rough dim-less th. sca. tplus : 0.24592E+00 0.10349E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.91215E-04 116 0.27635E+00 0.30122E-02 0.62416E+00 c Velocity[X] 0.52292E-03 c Velocity[Y] 0.24893E-02 c Velocity[Z] 0.44274E-29 c Pressure 0.36747E-03 11 0.41580E-07 0.82057E-01 0.14829E-02 c TempK 0.37832E+02 88 0.67981E-03 0.15359E-01 0.41018E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21104 0.23226 -4.9697e-006 -4.9697e-006 v Velocity[Y] -0.31865 0.88176 0.011862 0.011862 v Velocity[Z] -5.1005e-014 5.7197e-014 -1.2946e-016 -1.2946e-016 v ǁVelocityǁ 0.00088028 0.88176 0.075908 0.075908 v Pressure -1.0072 1.0066 -4.2633e-016 1.5179e-016 v TempK 292.59 306.68 295.06 295.06 v Density 1 1 1 1 v CourantNb 0.35609 8 7.4862 7.4862 v FourierNb 0.13005 5.2827 0.708 0.708 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2776 11.276 1.5332 1.5332 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.55 306.16 295.11 295.1 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.61642 12.41 8.1942 8.1942 INSTANT 0.147000000E+02 TIME STEP NUMBER 147 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.89898E-03 0.46679E-01 Friction velocity uk : 0.89898E-03 0.46679E-01 Dimensionless distance yplus : 0.30703E+00 0.15942E+02 Friction thermal sca. tstar : -0.69874E+01 0.21239E+01 Rough dim-less th. sca. tplus : 0.21798E+00 0.11319E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97903E-04 115 0.28471E+00 0.31852E-02 0.66642E+00 c Velocity[X] 0.54918E-03 c Velocity[Y] 0.26360E-02 c Velocity[Z] 0.46995E-29 c Pressure 0.36702E-03 11 0.41932E-07 0.79746E-01 0.15950E-02 c TempK 0.38086E+02 87 0.63422E-03 0.12755E-01 0.38356E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20407 0.22111 7.5571e-007 7.5571e-007 v Velocity[Y] -0.28525 0.94032 0.011447 0.011447 v Velocity[Z] -5.2012e-014 5.9292e-014 -1.3085e-016 -1.3085e-016 v ǁVelocityǁ 0.00053034 0.94033 0.075708 0.075708 v Pressure -1.0079 1.0066 -4.1744e-016 1.0842e-016 v TempK 292.58 306.35 295.08 295.08 v Density 1 1 1 1 v CourantNb 0.68394 8 7.5082 7.5082 v FourierNb 0.11724 5.597 0.70318 0.70318 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25025 11.947 1.5236 1.5236 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.59 306.68 295.12 295.1 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0748 13.27 8.2114 8.2114 INSTANT 0.148000000E+02 TIME STEP NUMBER 148 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.15541E-02 0.42631E-01 Friction velocity uk : 0.15541E-02 0.42631E-01 Dimensionless distance yplus : 0.53076E+00 0.14560E+02 Friction thermal sca. tstar : -0.56079E+01 0.14726E+01 Rough dim-less th. sca. tplus : 0.37683E+00 0.10337E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96687E-04 115 0.28311E+00 0.28632E-02 0.62331E+00 c Velocity[X] 0.49368E-03 c Velocity[Y] 0.23695E-02 c Velocity[Z] 0.51969E-29 c Pressure 0.33744E-03 11 0.44251E-07 0.72841E-01 0.13051E-02 c TempK 0.38276E+02 86 0.61077E-03 0.13471E-01 0.39278E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21672 0.2022 -1.6005e-005 -1.6005e-005 v Velocity[Y] -0.29837 0.92547 0.01138 0.01138 v Velocity[Z] -5.7745e-014 5.6006e-014 -1.2467e-016 -1.2467e-016 v ǁVelocityǁ 0.00039191 0.92815 0.075262 0.075262 v Pressure -1.0078 1.0052 -1.0125e-015 -3.4694e-016 v TempK 292.52 306.22 295.09 295.09 v Density 1 1 1 1 v CourantNb 0.53977 8 7.4724 7.4724 v FourierNb 0.123 5.1961 0.69688 0.69688 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26256 11.602 1.5108 1.5108 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.58 306.35 295.13 295.12 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.3879 13.196 8.1693 8.1693 INSTANT 0.149000000E+02 TIME STEP NUMBER 149 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.59287E-03 0.45047E-01 Friction velocity uk : 0.59287E-03 0.45047E-01 Dimensionless distance yplus : 0.20248E+00 0.15385E+02 Friction thermal sca. tstar : -0.32771E+02 0.61286E+01 Rough dim-less th. sca. tplus : 0.14376E+00 0.10923E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.95351E-04 116 0.26122E+00 0.28066E-02 0.60390E+00 c Velocity[X] 0.50255E-03 c Velocity[Y] 0.23040E-02 c Velocity[Z] 0.52663E-29 c Pressure 0.35981E-03 10 0.43650E-07 0.79849E-01 0.11858E-02 c TempK 0.38290E+02 85 0.72799E-03 0.12575E-01 0.37811E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21749 0.18128 -1.4932e-006 -1.4932e-006 v Velocity[Y] -0.28636 0.94558 0.011479 0.011479 v Velocity[Z] -5.9064e-014 5.0249e-014 -1.1276e-016 -1.1276e-016 v ǁVelocityǁ 0.00058813 0.94566 0.075479 0.075479 v Pressure -1.009 1.0053 -2.7534e-016 3.4694e-016 v TempK 292.45 306.7 295.1 295.1 v Density 1 1 1 1 v CourantNb 0.12893 8 7.4073 7.4073 v FourierNb 0.13215 4.1667 0.69214 0.69214 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28208 10.329 1.501 1.501 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.52 306.22 295.14 295.13 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.40183 12.167 8.0995 8.0995 INSTANT 0.150000000E+02 TIME STEP NUMBER 150 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.25879E-03 0.42244E-01 Friction velocity uk : 0.25879E-03 0.42244E-01 Dimensionless distance yplus : 0.88384E-01 0.14428E+02 Friction thermal sca. tstar : -0.11327E+02 0.41860E+01 Rough dim-less th. sca. tplus : 0.62751E-01 0.10243E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96301E-04 116 0.24810E+00 0.30129E-02 0.63582E+00 c Velocity[X] 0.52596E-03 c Velocity[Y] 0.24870E-02 c Velocity[Z] 0.56217E-29 c Pressure 0.35559E-03 15 0.50337E-07 0.77880E-01 0.12269E-02 c TempK 0.38313E+02 84 0.55212E-03 0.94206E-02 0.33772E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19948 0.21549 -2.6594e-005 -2.6594e-005 v Velocity[Y] -0.24002 0.91071 0.011402 0.011402 v Velocity[Z] -5.8265e-014 5.6634e-014 -1.1059e-016 -1.1059e-016 v ǁVelocityǁ 0.0007426 0.9125 0.074996 0.074996 v Pressure -1.0101 1.007 -4.5297e-016 1.5179e-016 v TempK 292.39 306.78 295.12 295.12 v Density 1 1 1 1 v CourantNb 0.25466 8 7.3782 7.3782 v FourierNb 0.12457 3.9921 0.69158 0.69158 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26591 11.362 1.5007 1.5007 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.45 306.7 295.16 295.15 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.62224 11.917 8.0698 8.0698 INSTANT 0.151000000E+02 TIME STEP NUMBER 151 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.65949E-03 0.46482E-01 Friction velocity uk : 0.65949E-03 0.46482E-01 Dimensionless distance yplus : 0.22524E+00 0.15875E+02 Friction thermal sca. tstar : -0.19466E+02 0.25539E+01 Rough dim-less th. sca. tplus : 0.15991E+00 0.11271E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96381E-04 116 0.24243E+00 0.30212E-02 0.62795E+00 c Velocity[X] 0.51253E-03 c Velocity[Y] 0.25087E-02 c Velocity[Z] 0.53899E-29 c Pressure 0.33986E-03 11 0.45748E-07 0.72932E-01 0.12054E-02 c TempK 0.38276E+02 82 0.56550E-03 0.11889E-01 0.36072E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19656 0.20744 -4.1812e-006 -4.1812e-006 v Velocity[Y] -0.29 1.0965 0.011463 0.011463 v Velocity[Z] -5.937e-014 5.7882e-014 -1.0798e-016 -1.0798e-016 v ǁVelocityǁ 0.00046169 1.1061 0.074325 0.074325 v Pressure -1.012 1.0063 -1.4655e-015 -8.5652e-016 v TempK 292.36 306.5 295.14 295.14 v Density 1 1 1 1 v CourantNb 0.25702 8 7.3304 7.3304 v FourierNb 0.13703 4.3913 0.69708 0.69708 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2925 12.498 1.5141 1.5141 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.39 306.78 295.17 295.16 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.59279 11.207 8.0275 8.0275 INSTANT 0.152000000E+02 TIME STEP NUMBER 152 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.80578E-03 0.43213E-01 Friction velocity uk : 0.80578E-03 0.43213E-01 Dimensionless distance yplus : 0.27520E+00 0.14759E+02 Friction thermal sca. tstar : -0.70110E+01 0.25089E+01 Rough dim-less th. sca. tplus : 0.19539E+00 0.10478E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.99905E-04 115 0.24072E+00 0.30570E-02 0.62780E+00 c Velocity[X] 0.54265E-03 c Velocity[Y] 0.25144E-02 c Velocity[Z] 0.53450E-29 c Pressure 0.36601E-03 11 0.43423E-07 0.77217E-01 0.13592E-02 c TempK 0.38266E+02 84 0.62165E-03 0.12028E-01 0.37546E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17092 0.21388 -2.8293e-005 -2.8293e-005 v Velocity[Y] -0.25868 0.98044 0.011495 0.011495 v Velocity[Z] -5.5434e-014 5.4833e-014 -1.1351e-016 -1.1351e-016 v ǁVelocityǁ 0.00070835 0.98047 0.07443 0.07443 v Pressure -1.0135 1.0073 1.2168e-015 1.7998e-015 v TempK 292.37 305.71 295.16 295.16 v Density 1 1 1 1 v CourantNb 0.44655 8 7.2412 7.2412 v FourierNb 0.13542 4.8304 0.70673 0.70673 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28907 13.748 1.5364 1.5364 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.36 306.5 295.19 295.18 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.8207 10.814 7.9479 7.9479 INSTANT 0.153000000E+02 TIME STEP NUMBER 153 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13285E-02 0.43609E-01 Friction velocity uk : 0.13285E-02 0.43609E-01 Dimensionless distance yplus : 0.45372E+00 0.14894E+02 Friction thermal sca. tstar : -0.10116E+02 0.30847E+01 Rough dim-less th. sca. tplus : 0.32214E+00 0.10574E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10239E-03 115 0.25118E+00 0.31756E-02 0.66341E+00 c Velocity[X] 0.61122E-03 c Velocity[Y] 0.25643E-02 c Velocity[Z] 0.57656E-29 c Pressure 0.34930E-03 11 0.39866E-07 0.71259E-01 0.15164E-02 c TempK 0.38419E+02 82 0.56927E-03 0.15461E-01 0.41946E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19743 0.20702 -2.7209e-006 -2.7209e-006 v Velocity[Y] -0.28496 0.88979 0.011165 0.011165 v Velocity[Z] -5.6652e-014 5.6618e-014 -1.1436e-016 -1.1436e-016 v ǁVelocityǁ 0.0003388 0.89257 0.073614 0.073614 v Pressure -1.0133 1.0065 -4.4409e-017 5.2042e-016 v TempK 292.41 304.94 295.17 295.17 v Density 1 1 1 1 v CourantNb 0.37045 8 7.221 7.221 v FourierNb 0.13479 5.3134 0.71723 0.71723 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28772 15.123 1.5602 1.5602 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.37 305.71 295.21 295.2 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0669 10.577 7.9382 7.9382 INSTANT 0.154000000E+02 TIME STEP NUMBER 154 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.66801E-03 0.43570E-01 Friction velocity uk : 0.66801E-03 0.43570E-01 Dimensionless distance yplus : 0.22815E+00 0.14880E+02 Friction thermal sca. tstar : -0.91689E+01 0.12227E+01 Rough dim-less th. sca. tplus : 0.16198E+00 0.10565E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.99540E-04 115 0.23749E+00 0.28794E-02 0.62190E+00 c Velocity[X] 0.50696E-03 c Velocity[Y] 0.23725E-02 c Velocity[Z] 0.53875E-29 c Pressure 0.32038E-03 11 0.39109E-07 0.64253E-01 0.14211E-02 c TempK 0.38382E+02 84 0.63187E-03 0.19312E-01 0.44260E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20653 0.21125 -5.709e-006 -5.709e-006 v Velocity[Y] -0.32477 0.92466 0.011379 0.011379 v Velocity[Z] -5.9818e-014 5.4793e-014 -1.1287e-016 -1.1287e-016 v ǁVelocityǁ 0.00075128 0.9254 0.074149 0.074149 v Pressure -1.0125 1.0059 -6.9278e-016 4.3368e-017 v TempK 292.47 304.42 295.19 295.19 v Density 1 1 1 1 v CourantNb 0.19806 8 7.1912 7.1912 v FourierNb 0.14567 5.0114 0.73274 0.73274 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31094 14.263 1.5948 1.5948 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.41 304.94 295.23 295.22 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.63339 12.899 7.924 7.924 INSTANT 0.155000000E+02 TIME STEP NUMBER 155 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.87794E-03 0.45442E-01 Friction velocity uk : 0.87794E-03 0.45442E-01 Dimensionless distance yplus : 0.29984E+00 0.15520E+02 Friction thermal sca. tstar : -0.15624E+02 0.20521E+01 Rough dim-less th. sca. tplus : 0.21288E+00 0.11019E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10040E-03 115 0.23479E+00 0.28814E-02 0.61255E+00 c Velocity[X] 0.45528E-03 c Velocity[Y] 0.24261E-02 c Velocity[Z] 0.52516E-29 c Pressure 0.33646E-03 12 0.34736E-07 0.66748E-01 0.12568E-02 c TempK 0.38362E+02 86 0.57871E-03 0.17490E-01 0.44748E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18037 0.21028 1.03e-005 1.03e-005 v Velocity[Y] -0.31752 0.89208 0.011383 0.011383 v Velocity[Z] -5.7171e-014 5.6097e-014 -1.2867e-016 -1.2867e-016 v ǁVelocityǁ 0.00033282 0.89418 0.074113 0.074113 v Pressure -1.0117 1.0056 -3.0198e-016 4.12e-016 v TempK 292.53 303.29 295.21 295.21 v Density 1 1 1 1 v CourantNb 0.13396 8 7.2279 7.2279 v FourierNb 0.12986 3.8484 0.73661 0.73661 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27719 10.953 1.6003 1.6003 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.47 304.42 295.25 295.24 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.55608 11.775 7.9645 7.9645 INSTANT 0.156000000E+02 TIME STEP NUMBER 156 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.57745E-03 0.43037E-01 Friction velocity uk : 0.57745E-03 0.43037E-01 Dimensionless distance yplus : 0.19722E+00 0.14698E+02 Friction thermal sca. tstar : -0.11779E+02 0.92074E-01 Rough dim-less th. sca. tplus : 0.14002E+00 0.10436E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10224E-03 115 0.23614E+00 0.30835E-02 0.63485E+00 c Velocity[X] 0.48435E-03 c Velocity[Y] 0.25991E-02 c Velocity[Z] 0.49858E-29 c Pressure 0.34542E-03 11 0.35095E-07 0.67221E-01 0.11358E-02 c TempK 0.38262E+02 86 0.60574E-03 0.21808E-01 0.48034E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17218 0.20812 2.9652e-006 2.9652e-006 v Velocity[Y] -0.31478 0.97359 0.011395 0.011395 v Velocity[Z] -5.8321e-014 6.5828e-014 -1.2879e-016 -1.2879e-016 v ǁVelocityǁ 0.00041037 0.97433 0.074749 0.074749 v Pressure -1.0121 1.0063 -8.6153e-016 -2.7105e-016 v TempK 292.56 302.6 295.22 295.22 v Density 1 1 1 1 v CourantNb 0.41036 8 7.2424 7.2424 v FourierNb 0.11872 3.7943 0.74052 0.74052 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25341 10.799 1.6078 1.6078 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.53 303.29 295.26 295.25 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75819 11.393 7.9829 7.9829 INSTANT 0.157000000E+02 TIME STEP NUMBER 157 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.98627E-04 0.45605E-01 Friction velocity uk : 0.98627E-04 0.45605E-01 Dimensionless distance yplus : 0.33684E-01 0.15576E+02 Friction thermal sca. tstar : -0.20353E+03 0.00000E+00 Rough dim-less th. sca. tplus : 0.23915E-01 0.11058E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10349E-03 115 0.24057E+00 0.31958E-02 0.65923E+00 c Velocity[X] 0.52094E-03 c Velocity[Y] 0.26749E-02 c Velocity[Z] 0.53768E-29 c Pressure 0.33026E-03 12 0.36390E-07 0.62320E-01 0.10595E-02 c TempK 0.38307E+02 88 0.60015E-03 0.20127E-01 0.47147E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17789 0.21507 6.0308e-006 6.0308e-006 v Velocity[Y] -0.26927 0.87384 0.011177 0.011177 v Velocity[Z] -6.3835e-014 6.4686e-014 -1.3711e-016 -1.3711e-016 v ǁVelocityǁ 0.00018613 0.87437 0.074506 0.074506 v Pressure -1.0111 1.0067 -3.9968e-016 7.5894e-017 v TempK 292.57 302.58 295.23 295.23 v Density 1 1 1 1 v CourantNb 0.27339 8 7.2909 7.2909 v FourierNb 0.12021 4.1737 0.73828 0.73828 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2566 11.879 1.6027 1.6027 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.56 303.15 295.27 295.26 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.62806 11.75 8.0291 8.0291 INSTANT 0.158000000E+02 TIME STEP NUMBER 158 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13547E-02 0.43234E-01 Friction velocity uk : 0.13547E-02 0.43234E-01 Dimensionless distance yplus : 0.46268E+00 0.14766E+02 Friction thermal sca. tstar : -0.11573E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.32850E+00 0.10483E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10024E-03 116 0.23087E+00 0.30392E-02 0.64484E+00 c Velocity[X] 0.49996E-03 c Velocity[Y] 0.25393E-02 c Velocity[Z] 0.46096E-29 c Pressure 0.32768E-03 11 0.29431E-07 0.57859E-01 0.10649E-02 c TempK 0.38218E+02 89 0.55935E-03 0.18436E-01 0.46201E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14247 0.22796 4.0311e-006 4.0311e-006 v Velocity[Y] -0.25933 0.98379 0.011103 0.011103 v Velocity[Z] -6.6559e-014 6.5251e-014 -1.3431e-016 -1.3431e-016 v ǁVelocityǁ 0.00046945 0.98379 0.075162 0.075162 v Pressure -1.0097 1.0073 -3.0198e-016 3.2526e-016 v TempK 292.59 302.49 295.23 295.23 v Density 1 1 1 1 v CourantNb 0.33497 8 7.2846 7.2846 v FourierNb 0.12602 4.5911 0.73941 0.73941 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26901 13.067 1.605 1.605 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.57 303.15 295.28 295.27 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67186 11.656 8.024 8.024 INSTANT 0.159000000E+02 TIME STEP NUMBER 159 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.53077E-03 0.43130E-01 Friction velocity uk : 0.53077E-03 0.43130E-01 Dimensionless distance yplus : 0.18127E+00 0.14730E+02 Friction thermal sca. tstar : -0.78737E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.12870E+00 0.10458E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.10092E-03 116 0.23183E+00 0.29604E-02 0.63276E+00 c Velocity[X] 0.47863E-03 c Velocity[Y] 0.24817E-02 c Velocity[Z] 0.49599E-29 c Pressure 0.32416E-03 11 0.30415E-07 0.54085E-01 0.10283E-02 c TempK 0.38211E+02 89 0.52097E-03 0.17135E-01 0.43361E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17877 0.23378 1.1435e-005 1.1435e-005 v Velocity[Y] -0.34172 0.8968 0.011013 0.011013 v Velocity[Z] -6.5088e-014 5.1115e-014 -1.6075e-016 -1.6075e-016 v ǁVelocityǁ 0.00016254 0.89813 0.075403 0.075403 v Pressure -1.0091 1.0062 -9.4147e-016 -4.0115e-016 v TempK 292.59 302.83 295.24 295.24 v Density 1 1 1 1 v CourantNb 0.2915 8 7.3472 7.3472 v FourierNb 0.13071 5.0502 0.73459 0.73459 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27902 14.373 1.5953 1.5953 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.59 303.15 295.29 295.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.50029 11.839 8.0818 8.0818 INSTANT 0.160000000E+02 TIME STEP NUMBER 160 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.16393E-03 0.42278E-01 Friction velocity uk : 0.16393E-03 0.42278E-01 Dimensionless distance yplus : 0.55988E-01 0.14439E+02 Friction thermal sca. tstar : -0.50032E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.39751E-01 0.10252E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98354E-04 117 0.23274E+00 0.28041E-02 0.60728E+00 c Velocity[X] 0.49226E-03 c Velocity[Y] 0.23118E-02 c Velocity[Z] 0.49144E-29 c Pressure 0.33605E-03 11 0.29746E-07 0.55830E-01 0.10981E-02 c TempK 0.38125E+02 89 0.49062E-03 0.15995E-01 0.41547E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14171 0.2347 5.8797e-006 5.8797e-006 v Velocity[Y] -0.35249 0.93338 0.011155 0.011155 v Velocity[Z] -6.0302e-014 6.8411e-014 -1.4882e-016 -1.4882e-016 v ǁVelocityǁ 9.4587e-005 0.93437 0.075942 0.075942 v Pressure -1.0081 1.0073 4.6185e-016 1.0734e-015 v TempK 292.58 303.29 295.24 295.24 v Density 1 1 1 1 v CourantNb 0.23795 8 7.382 7.382 v FourierNb 0.11585 5.5552 0.72933 0.72933 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29369 15.811 1.5852 1.5852 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.59 303.15 295.29 295.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.86136 11.791 8.1113 8.1113 INSTANT 0.161000000E+02 TIME STEP NUMBER 161 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.49393E-03 0.43829E-01 Friction velocity uk : 0.49393E-03 0.43829E-01 Dimensionless distance yplus : 0.16869E+00 0.14969E+02 Friction thermal sca. tstar : -0.57943E+01 0.24904E+00 Rough dim-less th. sca. tplus : 0.11977E+00 0.10628E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98601E-04 117 0.23593E+00 0.29135E-02 0.62636E+00 c Velocity[X] 0.48624E-03 c Velocity[Y] 0.24273E-02 c Velocity[Z] 0.55343E-29 c Pressure 0.32339E-03 11 0.36024E-07 0.56132E-01 0.11963E-02 c TempK 0.38167E+02 89 0.48018E-03 0.14246E-01 0.38857E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14754 0.23249 6.5381e-006 6.5381e-006 v Velocity[Y] -0.31096 0.86077 0.011053 0.011053 v Velocity[Z] -6.1078e-014 5.5559e-014 -1.3405e-016 -1.3405e-016 v ǁVelocityǁ 0.0001231 0.86084 0.076048 0.076048 v Pressure -1.0063 1.0059 -1.4122e-015 -8.5652e-016 v TempK 292.56 303.73 295.24 295.24 v Density 1 1 1 1 v CourantNb 0.45737 8 7.4031 7.4031 v FourierNb 0.12744 4.2727 0.72553 0.72553 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29183 10.915 1.5775 1.5775 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.58 303.29 295.29 295.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89376 11.835 8.1286 8.1286 INSTANT 0.162000000E+02 TIME STEP NUMBER 162 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.54269E-03 0.38717E-01 Friction velocity uk : 0.54269E-03 0.38717E-01 Dimensionless distance yplus : 0.18534E+00 0.13223E+02 Friction thermal sca. tstar : -0.58698E+01 0.13951E+01 Rough dim-less th. sca. tplus : 0.13159E+00 0.93882E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.95404E-04 117 0.23775E+00 0.27683E-02 0.59930E+00 c Velocity[X] 0.43234E-03 c Velocity[Y] 0.23359E-02 c Velocity[Z] 0.51594E-29 c Pressure 0.31811E-03 12 0.26844E-07 0.55722E-01 0.10710E-02 c TempK 0.38200E+02 89 0.42100E-03 0.13866E-01 0.38056E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14143 0.24566 -1.2569e-005 -1.2569e-005 v Velocity[Y] -0.26462 0.92496 0.011219 0.011219 v Velocity[Z] -6.0214e-014 6.1759e-014 -1.286e-016 -1.286e-016 v ǁVelocityǁ 0.00043602 0.92521 0.076475 0.076475 v Pressure -1.0046 1.0067 3.0198e-016 8.9989e-016 v TempK 292.54 303.93 295.24 295.24 v Density 1 1 1 1 v CourantNb 0.02121 8 7.4455 7.4455 v FourierNb 0.14018 4.6999 0.71976 0.71976 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3005 10.249 1.5646 1.5646 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.56 303.73 295.29 295.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85631 12.557 8.1652 8.1652 INSTANT 0.163000000E+02 TIME STEP NUMBER 163 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.75582E-03 0.42689E-01 Friction velocity uk : 0.75582E-03 0.42689E-01 Dimensionless distance yplus : 0.25814E+00 0.14580E+02 Friction thermal sca. tstar : -0.91771E+01 0.68275E+00 Rough dim-less th. sca. tplus : 0.18327E+00 0.10351E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.93272E-04 117 0.22677E+00 0.27928E-02 0.59865E+00 c Velocity[X] 0.43469E-03 c Velocity[Y] 0.23581E-02 c Velocity[Z] 0.51177E-29 c Pressure 0.33485E-03 11 0.28464E-07 0.58641E-01 0.10737E-02 c TempK 0.38306E+02 89 0.44172E-03 0.12833E-01 0.37316E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15985 0.25251 2.3089e-006 2.3089e-006 v Velocity[Y] -0.27341 0.91191 0.011332 0.011332 v Velocity[Z] -6.0956e-014 5.13e-014 -1.2962e-016 -1.2962e-016 v ǁVelocityǁ 0.00074977 0.91191 0.076855 0.076855 v Pressure -1.0047 1.0063 -1.3323e-015 -7.0473e-016 v TempK 292.52 304.28 295.24 295.24 v Density 1 1 1 1 v CourantNb 0.54262 8 7.4175 7.4175 v FourierNb 0.14994 5.1699 0.71764 0.71764 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32005 11.036 1.5589 1.5589 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.54 303.93 295.29 295.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1973 12.786 8.1351 8.1351 INSTANT 0.164000000E+02 TIME STEP NUMBER 164 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.90816E-03 0.40006E-01 Friction velocity uk : 0.90816E-03 0.40006E-01 Dimensionless distance yplus : 0.31017E+00 0.13663E+02 Friction thermal sca. tstar : -0.62990E+01 0.15671E+01 Rough dim-less th. sca. tplus : 0.22021E+00 0.97008E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96080E-04 116 0.23884E+00 0.28689E-02 0.61714E+00 c Velocity[X] 0.43543E-03 c Velocity[Y] 0.24335E-02 c Velocity[Z] 0.47062E-29 c Pressure 0.33258E-03 11 0.28315E-07 0.60589E-01 0.10673E-02 c TempK 0.38407E+02 89 0.46104E-03 0.13739E-01 0.38852E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18288 0.24937 -2.5358e-005 -2.5358e-005 v Velocity[Y] -0.27286 0.8168 0.011126 0.011126 v Velocity[Z] -6.1509e-014 5.0457e-014 -1.3956e-016 -1.3956e-016 v ǁVelocityǁ 0.00057771 0.81758 0.076904 0.076904 v Pressure -1.0046 1.0066 -1.581e-015 -9.6494e-016 v TempK 292.49 304.36 295.25 295.25 v Density 1 1 1 1 v CourantNb 0.33835 8 7.4778 7.4778 v FourierNb 0.14426 5.4295 0.7124 0.7124 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34374 11.59 1.5456 1.5456 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.52 304.28 295.3 295.29 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.56646 13.009 8.1902 8.1902 INSTANT 0.165000000E+02 TIME STEP NUMBER 165 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14459E-03 0.43659E-01 Friction velocity uk : 0.14459E-03 0.43659E-01 Dimensionless distance yplus : 0.49383E-01 0.14911E+02 Friction thermal sca. tstar : -0.91881E+01 0.34609E+02 Rough dim-less th. sca. tplus : 0.35061E-01 0.10586E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94020E-04 116 0.23674E+00 0.26651E-02 0.59015E+00 c Velocity[X] 0.42332E-03 c Velocity[Y] 0.22417E-02 c Velocity[Z] 0.44863E-29 c Pressure 0.31953E-03 11 0.30269E-07 0.62535E-01 0.11819E-02 c TempK 0.38480E+02 88 0.51462E-03 0.13696E-01 0.39773E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19814 0.23642 -6.4342e-006 -6.4342e-006 v Velocity[Y] -0.24885 0.82509 0.011155 0.011155 v Velocity[Z] -5.0458e-014 5.0654e-014 -1.3042e-016 -1.3042e-016 v ǁVelocityǁ 0.00060574 0.82564 0.07673 0.07673 v Pressure -1.0043 1.0063 -1.5721e-015 -9.3241e-016 v TempK 292.46 304.4 295.25 295.25 v Density 1 1 1 1 v CourantNb 0.50839 8 7.4565 7.4565 v FourierNb 0.14086 5.1825 0.71008 0.71008 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30066 11.105 1.5408 1.5408 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.49 304.36 295.3 295.29 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0033 12.456 8.1666 8.1666 INSTANT 0.166000000E+02 TIME STEP NUMBER 166 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.70563E-03 0.40835E-01 Friction velocity uk : 0.70563E-03 0.40835E-01 Dimensionless distance yplus : 0.24099E+00 0.13947E+02 Friction thermal sca. tstar : -0.57813E+01 0.21960E+01 Rough dim-less th. sca. tplus : 0.17110E+00 0.99018E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.93359E-04 116 0.23484E+00 0.27510E-02 0.60100E+00 c Velocity[X] 0.44492E-03 c Velocity[Y] 0.23061E-02 c Velocity[Z] 0.39646E-29 c Pressure 0.33329E-03 11 0.30407E-07 0.66456E-01 0.11954E-02 c TempK 0.38428E+02 87 0.49808E-03 0.16279E-01 0.43002E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21468 0.21606 -3.7806e-005 -3.7806e-005 v Velocity[Y] -0.22906 0.88552 0.011217 0.011217 v Velocity[Z] -4.7411e-014 6.0446e-014 -1.2361e-016 -1.2361e-016 v ǁVelocityǁ 0.00051012 0.88555 0.077114 0.077114 v Pressure -1.004 1.0072 1.5987e-016 7.1557e-016 v TempK 292.44 304.4 295.26 295.26 v Density 1 1 1 1 v CourantNb 0.11813 8 7.4483 7.4483 v FourierNb 0.15494 5.1678 0.71537 0.71537 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33073 11.161 1.5519 1.5519 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.46 304.4 295.31 295.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.83732 12.982 8.1637 8.1637 INSTANT 0.167000000E+02 TIME STEP NUMBER 167 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.97180E-03 0.42792E-01 Friction velocity uk : 0.97180E-03 0.42792E-01 Dimensionless distance yplus : 0.33190E+00 0.14615E+02 Friction thermal sca. tstar : -0.13418E+02 0.29287E+01 Rough dim-less th. sca. tplus : 0.23564E+00 0.10376E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96670E-04 115 0.25447E+00 0.29565E-02 0.62846E+00 c Velocity[X] 0.43967E-03 c Velocity[Y] 0.25168E-02 c Velocity[Z] 0.41676E-29 c Pressure 0.33233E-03 11 0.29964E-07 0.66585E-01 0.11056E-02 c TempK 0.38489E+02 87 0.47876E-03 0.15601E-01 0.43269E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20229 0.21351 -1.7957e-005 -1.7957e-005 v Velocity[Y] -0.23787 0.91527 0.011038 0.011038 v Velocity[Z] -4.5878e-014 5.0478e-014 -1.0753e-016 -1.0753e-016 v ǁVelocityǁ 0.00026947 0.91557 0.076514 0.076514 v Pressure -1.0035 1.0063 -2.6645e-017 6.18e-016 v TempK 292.4 304.3 295.26 295.26 v Density 1 1 1 1 v CourantNb 0.66272 8 7.5016 7.5016 v FourierNb 0.14727 5.3477 0.71513 0.71513 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31437 12.278 1.5519 1.5519 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.44 304.4 295.31 295.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99016 13.348 8.2167 8.2167 INSTANT 0.168000000E+02 TIME STEP NUMBER 168 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11509E-02 0.41561E-01 Friction velocity uk : 0.11509E-02 0.41561E-01 Dimensionless distance yplus : 0.39307E+00 0.14194E+02 Friction thermal sca. tstar : -0.46091E+01 0.19405E+01 Rough dim-less th. sca. tplus : 0.27908E+00 0.10078E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94405E-04 115 0.25200E+00 0.27973E-02 0.60489E+00 c Velocity[X] 0.42050E-03 c Velocity[Y] 0.23768E-02 c Velocity[Z] 0.42283E-29 c Pressure 0.32623E-03 12 0.29525E-07 0.65989E-01 0.10833E-02 c TempK 0.38528E+02 88 0.46006E-03 0.15496E-01 0.41065E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22982 0.21113 -3.7602e-005 -3.7602e-005 v Velocity[Y] -0.24407 0.97764 0.011216 0.011216 v Velocity[Z] -5.0442e-014 4.9565e-014 -1.2285e-016 -1.2285e-016 v ǁVelocityǁ 0.00024226 0.97806 0.077108 0.077108 v Pressure -1.0032 1.0065 -4.7962e-016 1.0842e-016 v TempK 292.38 304.24 295.27 295.27 v Density 1 1 1 1 v CourantNb 0.48424 8 7.4646 7.4646 v FourierNb 0.13985 4.7496 0.71678 0.71678 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32271 13.505 1.5558 1.5558 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.4 304.3 295.32 295.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.90976 12.517 8.1813 8.1813 INSTANT 0.169000000E+02 TIME STEP NUMBER 169 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32670E-03 0.43157E-01 Friction velocity uk : 0.32670E-03 0.43157E-01 Dimensionless distance yplus : 0.11158E+00 0.14740E+02 Friction thermal sca. tstar : -0.61784E+01 0.96051E+00 Rough dim-less th. sca. tplus : 0.79217E-01 0.10465E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98011E-04 117 0.25295E+00 0.30316E-02 0.63844E+00 c Velocity[X] 0.47416E-03 c Velocity[Y] 0.25574E-02 c Velocity[Z] 0.41859E-29 c Pressure 0.33107E-03 11 0.29949E-07 0.66369E-01 0.12524E-02 c TempK 0.38656E+02 88 0.54941E-03 0.17510E-01 0.44260E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.2112 0.21708 -3.2832e-006 -3.2832e-006 v Velocity[Y] -0.24812 0.91301 0.011055 0.011055 v Velocity[Z] -5.4096e-014 4.9145e-014 -1.1516e-016 -1.1516e-016 v ǁVelocityǁ 0.00049776 0.91408 0.077066 0.077066 v Pressure -1.0029 1.0079 -1.7586e-015 -1.1926e-015 v TempK 292.38 304.18 295.27 295.27 v Density 1 1 1 1 v CourantNb 0.36879 8 7.5172 7.5172 v FourierNb 0.13851 5.2197 0.71183 0.71183 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30974 14.856 1.5446 1.5446 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.38 304.24 295.32 295.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.96786 12.154 8.229 8.229 INSTANT 0.170000000E+02 TIME STEP NUMBER 170 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10159E-02 0.38355E-01 Friction velocity uk : 0.10159E-02 0.38355E-01 Dimensionless distance yplus : 0.34695E+00 0.13099E+02 Friction thermal sca. tstar : -0.16560E+02 0.32032E+01 Rough dim-less th. sca. tplus : 0.24633E+00 0.93003E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97874E-04 116 0.25254E+00 0.30450E-02 0.64552E+00 c Velocity[X] 0.49320E-03 c Velocity[Y] 0.25518E-02 c Velocity[Z] 0.41733E-29 c Pressure 0.34182E-03 12 0.31849E-07 0.66940E-01 0.13761E-02 c TempK 0.38756E+02 87 0.50836E-03 0.19772E-01 0.44169E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22087 0.21853 -3.6261e-005 -3.6261e-005 v Velocity[Y] -0.255 0.95397 0.010839 0.010839 v Velocity[Z] -5.612e-014 5.0122e-014 -1.2717e-016 -1.2717e-016 v ǁVelocityǁ 0.00031547 0.95544 0.07702 0.07702 v Pressure -1.0023 1.0069 -1.6076e-015 -9.7578e-016 v TempK 292.43 304.2 295.27 295.27 v Density 1 1 1 1 v CourantNb 0.50694 8 7.4584 7.4584 v FourierNb 0.14276 5.7417 0.71585 0.71585 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30865 16.341 1.554 1.554 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.38 304.18 295.32 295.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1956 13.166 8.1743 8.1743 INSTANT 0.171000000E+02 TIME STEP NUMBER 171 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.34211E-03 0.42571E-01 Friction velocity uk : 0.34211E-03 0.42571E-01 Dimensionless distance yplus : 0.11684E+00 0.14539E+02 Friction thermal sca. tstar : -0.45471E+01 0.10264E+01 Rough dim-less th. sca. tplus : 0.82956E-01 0.10323E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98054E-04 115 0.25432E+00 0.28475E-02 0.62981E+00 c Velocity[X] 0.47697E-03 c Velocity[Y] 0.23706E-02 c Velocity[Z] 0.45489E-29 c Pressure 0.32780E-03 11 0.30862E-07 0.64681E-01 0.14977E-02 c TempK 0.38865E+02 85 0.61539E-03 0.16025E-01 0.41644E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23025 0.22042 -1.7445e-005 -1.7445e-005 v Velocity[Y] -0.27199 0.87293 0.010743 0.010743 v Velocity[Z] -5.7164e-014 5.1842e-014 -1.0656e-016 -1.0656e-016 v ǁVelocityǁ 0.00031487 0.87758 0.076355 0.076355 v Pressure -1.0017 1.0073 -6.2172e-016 -1.0842e-017 v TempK 292.49 304.25 295.28 295.28 v Density 1 1 1 1 v CourantNb 0.37111 8 7.47 7.47 v FourierNb 0.14485 4.8362 0.7151 0.7151 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31155 11.897 1.5513 1.5513 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.43 304.2 295.33 295.32 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.6828 12.535 8.1851 8.1851 INSTANT 0.172000000E+02 TIME STEP NUMBER 172 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.19892E-03 0.41152E-01 Friction velocity uk : 0.19892E-03 0.41152E-01 Dimensionless distance yplus : 0.67937E-01 0.14055E+02 Friction thermal sca. tstar : -0.49588E+01 0.14312E+01 Rough dim-less th. sca. tplus : 0.48234E-01 0.99786E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96312E-04 115 0.25363E+00 0.28187E-02 0.61790E+00 c Velocity[X] 0.44021E-03 c Velocity[Y] 0.23784E-02 c Velocity[Z] 0.39630E-29 c Pressure 0.32718E-03 11 0.29807E-07 0.62446E-01 0.12501E-02 c TempK 0.38759E+02 84 0.47611E-03 0.13423E-01 0.37427E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21925 0.22344 -3.6827e-005 -3.6827e-005 v Velocity[Y] -0.25937 0.86155 0.010892 0.010892 v Velocity[Z] -6.1436e-014 5.3739e-014 -1.0786e-016 -1.0786e-016 v ǁVelocityǁ 0.00063511 0.86373 0.076191 0.076191 v Pressure -1.0011 1.0067 -1.7764e-017 5.2042e-016 v TempK 292.54 304.33 295.29 295.29 v Density 1 1 1 1 v CourantNb 0.59373 8 7.4444 7.4444 v FourierNb 0.13459 5.3138 0.72564 0.72564 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28729 13.086 1.5744 1.5744 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.49 304.25 295.33 295.32 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.83098 13.195 8.17 8.17 INSTANT 0.173000000E+02 TIME STEP NUMBER 173 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.63854E-03 0.43746E-01 Friction velocity uk : 0.63854E-03 0.43746E-01 Dimensionless distance yplus : 0.21808E+00 0.14941E+02 Friction thermal sca. tstar : -0.14597E+02 0.76415E+01 Rough dim-less th. sca. tplus : 0.15483E+00 0.10608E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96947E-04 114 0.24130E+00 0.28036E-02 0.61342E+00 c Velocity[X] 0.47794E-03 c Velocity[Y] 0.23257E-02 c Velocity[Z] 0.43773E-29 c Pressure 0.32403E-03 11 0.27471E-07 0.60221E-01 0.11623E-02 c TempK 0.38677E+02 85 0.54323E-03 0.13933E-01 0.38108E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24583 0.21839 -8.0085e-006 -8.0085e-006 v Velocity[Y] -0.25202 0.94435 0.011053 0.011053 v Velocity[Z] -6.0377e-014 5.4514e-014 -1.0241e-016 -1.0241e-016 v ǁVelocityǁ 0.00072102 0.94436 0.076586 0.076586 v Pressure -1.0012 1.0067 -4.9738e-016 5.421e-017 v TempK 292.54 304.51 295.3 295.3 v Density 1 1 1 1 v CourantNb 0.40417 8 7.4331 7.4331 v FourierNb 0.13038 5.8452 0.7338 0.7338 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27831 14.395 1.5927 1.5927 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.54 304.33 295.34 295.33 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72363 13.274 8.1669 8.1669 INSTANT 0.174000000E+02 TIME STEP NUMBER 174 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.82107E-03 0.43409E-01 Friction velocity uk : 0.82107E-03 0.43409E-01 Dimensionless distance yplus : 0.28042E+00 0.14825E+02 Friction thermal sca. tstar : -0.10800E+02 0.18016E+01 Rough dim-less th. sca. tplus : 0.19909E+00 0.10526E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.99303E-04 114 0.24302E+00 0.29878E-02 0.64151E+00 c Velocity[X] 0.50796E-03 c Velocity[Y] 0.24799E-02 c Velocity[Z] 0.47618E-29 c Pressure 0.31564E-03 11 0.28368E-07 0.58872E-01 0.11880E-02 c TempK 0.38777E+02 84 0.45242E-03 0.11643E-01 0.35411E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22929 0.22415 -1.539e-005 -1.539e-005 v Velocity[Y] -0.24139 0.85682 0.01105 0.01105 v Velocity[Z] -6.0067e-014 5.6364e-014 -1.1926e-016 -1.1926e-016 v ǁVelocityǁ 0.0012337 0.85751 0.076469 0.076469 v Pressure -1.0011 1.0075 -1.3944e-015 -7.3726e-016 v TempK 292.53 304.69 295.3 295.3 v Density 1 1 1 1 v CourantNb 0.34311 8 7.4849 7.4849 v FourierNb 0.11426 5.5059 0.73211 0.73211 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2439 14.213 1.5894 1.5894 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.54 304.51 295.35 295.34 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.84928 13.506 8.217 8.217 INSTANT 0.175000000E+02 TIME STEP NUMBER 175 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.20053E-02 0.44818E-01 Friction velocity uk : 0.20053E-02 0.44818E-01 Dimensionless distance yplus : 0.68489E+00 0.15307E+02 Friction thermal sca. tstar : -0.75221E+01 0.14372E+01 Rough dim-less th. sca. tplus : 0.48626E+00 0.10868E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98390E-04 113 0.22076E+00 0.28982E-02 0.61553E+00 c Velocity[X] 0.49697E-03 c Velocity[Y] 0.24012E-02 c Velocity[Z] 0.43293E-29 c Pressure 0.33370E-03 11 0.29584E-07 0.63881E-01 0.12347E-02 c TempK 0.38762E+02 84 0.55789E-03 0.11852E-01 0.35249E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19471 0.20155 3.504e-006 3.504e-006 v Velocity[Y] -0.25899 1.0069 0.011053 0.011053 v Velocity[Z] -5.5465e-014 5.6667e-014 -1.0428e-016 -1.0428e-016 v ǁVelocityǁ 0.00088697 1.0072 0.076562 0.076562 v Pressure -1.0013 1.0085 -5.6843e-016 5.421e-017 v TempK 292.54 304.84 295.32 295.32 v Density 1 1 1 1 v CourantNb 0.60569 8 7.4542 7.4542 v FourierNb 0.11445 4.8061 0.72946 0.72946 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.24431 13.679 1.5817 1.5817 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.53 304.69 295.36 295.35 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0637 12.806 8.1836 8.1836 INSTANT 0.176000000E+02 TIME STEP NUMBER 176 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.76186E-03 0.44578E-01 Friction velocity uk : 0.76186E-03 0.44578E-01 Dimensionless distance yplus : 0.26020E+00 0.15225E+02 Friction thermal sca. tstar : -0.46957E+01 0.14756E+01 Rough dim-less th. sca. tplus : 0.18474E+00 0.10809E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.99730E-04 113 0.23460E+00 0.31147E-02 0.64876E+00 c Velocity[X] 0.55425E-03 c Velocity[Y] 0.25604E-02 c Velocity[Z] 0.49795E-29 c Pressure 0.35033E-03 11 0.29607E-07 0.73378E-01 0.13547E-02 c TempK 0.38839E+02 84 0.54694E-03 0.10287E-01 0.34211E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.2144 0.20206 -2.1384e-005 -2.1384e-005 v Velocity[Y] -0.3077 0.90272 0.011103 0.011103 v Velocity[Z] -5.826e-014 5.7211e-014 -1.3689e-016 -1.3689e-016 v ǁVelocityǁ 0.00060524 0.90279 0.076622 0.076622 v Pressure -1.0009 1.0079 -1.7764e-017 5.8547e-016 v TempK 292.59 305 295.32 295.32 v Density 1 1 1 1 v CourantNb 0.35123 8 7.4486 7.4486 v FourierNb 0.1259 4.6347 0.72015 0.72015 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26874 13.191 1.5623 1.5623 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.54 304.84 295.37 295.36 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.5802 12.635 8.1687 8.1687 INSTANT 0.177000000E+02 TIME STEP NUMBER 177 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.22260E-02 0.42647E-01 Friction velocity uk : 0.22260E-02 0.42647E-01 Dimensionless distance yplus : 0.76024E+00 0.14565E+02 Friction thermal sca. tstar : -0.40345E+01 0.16795E+01 Rough dim-less th. sca. tplus : 0.53976E+00 0.10341E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.98753E-04 113 0.24125E+00 0.30963E-02 0.65300E+00 c Velocity[X] 0.56761E-03 c Velocity[Y] 0.25286E-02 c Velocity[Z] 0.49758E-29 c Pressure 0.34992E-03 11 0.28254E-07 0.75677E-01 0.13130E-02 c TempK 0.38833E+02 84 0.64640E-03 0.11042E-01 0.34480E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21261 0.18822 2.8161e-006 2.8161e-006 v Velocity[Y] -0.24596 0.85371 0.010788 0.010788 v Velocity[Z] -6.0302e-014 5.7435e-014 -1.0902e-016 -1.0902e-016 v ǁVelocityǁ 0.0011349 0.85379 0.076267 0.076267 v Pressure -1.0007 1.0096 8.8818e-017 6.3968e-016 v TempK 292.68 305.1 295.34 295.34 v Density 1 1 1 1 v CourantNb 0.28401 8 7.4506 7.4506 v FourierNb 0.12274 3.3271 0.72013 0.72013 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.262 9.0912 1.5613 1.5613 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.59 305 295.38 295.37 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.59547 11.327 8.1707 8.1707 INSTANT 0.178000000E+02 TIME STEP NUMBER 178 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.18134E-03 0.44502E-01 Friction velocity uk : 0.18134E-03 0.44502E-01 Dimensionless distance yplus : 0.61934E-01 0.15199E+02 Friction thermal sca. tstar : -0.34983E+01 0.27261E+01 Rough dim-less th. sca. tplus : 0.43972E-01 0.10791E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.96481E-04 112 0.23396E+00 0.28449E-02 0.60516E+00 c Velocity[X] 0.51162E-03 c Velocity[Y] 0.23333E-02 c Velocity[Z] 0.51339E-29 c Pressure 0.34577E-03 10 0.29146E-07 0.76255E-01 0.13385E-02 c TempK 0.38762E+02 84 0.45011E-03 0.98757E-02 0.33373E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.2453 0.18729 -9.6907e-007 -9.6907e-007 v Velocity[Y] -0.23068 0.87199 0.01097 0.01097 v Velocity[Z] -6.2135e-014 5.4749e-014 -1.2986e-016 -1.2986e-016 v ǁVelocityǁ 0.00034414 0.87199 0.076747 0.076747 v Pressure -1.0006 1.0092 -8.9706e-016 -2.4937e-016 v TempK 292.78 305.03 295.35 295.35 v Density 1 1 1 1 v CourantNb 0.17042 8 7.4618 7.4618 v FourierNb 0.13502 3.2277 0.7175 0.7175 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2882 8.8693 1.5551 1.5551 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.68 305.1 295.39 295.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69068 11.095 8.1793 8.1793 INSTANT 0.179000000E+02 TIME STEP NUMBER 179 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.50849E-03 0.44150E-01 Friction velocity uk : 0.50849E-03 0.44150E-01 Dimensionless distance yplus : 0.17366E+00 0.15079E+02 Friction thermal sca. tstar : -0.30189E+01 0.26725E+01 Rough dim-less th. sca. tplus : 0.12330E+00 0.10706E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97390E-04 112 0.23138E+00 0.29824E-02 0.62748E+00 c Velocity[X] 0.52388E-03 c Velocity[Y] 0.24585E-02 c Velocity[Z] 0.50426E-29 c Pressure 0.33705E-03 11 0.29451E-07 0.75897E-01 0.13528E-02 c TempK 0.38941E+02 85 0.61285E-03 0.10649E-01 0.34984E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22788 0.1838 -1.4038e-006 -1.4038e-006 v Velocity[Y] -0.23509 0.95585 0.011125 0.011125 v Velocity[Z] -6.1258e-014 5.2674e-014 -1.0991e-016 -1.0991e-016 v ǁVelocityǁ 0.00066672 0.95591 0.0772 0.0772 v Pressure -1 1.0098 -7.3719e-016 -1.4095e-016 v TempK 292.86 305.32 295.36 295.36 v Density 1 1 1 1 v CourantNb 0.38695 8 7.5002 7.5002 v FourierNb 0.12437 3.5505 0.70982 0.70982 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26547 8.6271 1.5387 1.5387 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.78 305.03 295.4 295.39 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73519 11.225 8.2101 8.2101 INSTANT 0.180000000E+02 TIME STEP NUMBER 180 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11082E-02 0.49288E-01 Friction velocity uk : 0.11082E-02 0.49288E-01 Dimensionless distance yplus : 0.37849E+00 0.16833E+02 Friction thermal sca. tstar : -0.26127E+01 0.11101E+01 Rough dim-less th. sca. tplus : 0.26872E+00 0.11951E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.95368E-04 113 0.23454E+00 0.30680E-02 0.63728E+00 c Velocity[X] 0.48604E-03 c Velocity[Y] 0.25819E-02 c Velocity[Z] 0.55008E-29 c Pressure 0.33795E-03 10 0.29093E-07 0.73620E-01 0.12527E-02 c TempK 0.39100E+02 84 0.53382E-03 0.10011E-01 0.34419E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17983 0.1591 -2.574e-005 -2.574e-005 v Velocity[Y] -0.28488 0.99809 0.011227 0.011227 v Velocity[Z] -6.2626e-014 6.2559e-014 -1.195e-016 -1.195e-016 v ǁVelocityǁ 0.00040344 1.0023 0.077006 0.077006 v Pressure -1.0002 1.0072 -1.3323e-015 -6.9389e-016 v TempK 292.92 305.6 295.37 295.37 v Density 1 1 1 1 v CourantNb 0.22316 8 7.4863 7.4863 v FourierNb 0.12951 3.9055 0.70376 0.70376 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27644 9.2684 1.5258 1.5258 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.86 305.32 295.41 295.4 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.47396 11.585 8.1901 8.1901 INSTANT 0.181000000E+02 TIME STEP NUMBER 181 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.42050E-03 0.50758E-01 Friction velocity uk : 0.42050E-03 0.50758E-01 Dimensionless distance yplus : 0.14361E+00 0.17336E+02 Friction thermal sca. tstar : -0.59850E+01 0.17491E+01 Rough dim-less th. sca. tplus : 0.10196E+00 0.12308E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97377E-04 113 0.24885E+00 0.29674E-02 0.62023E+00 c Velocity[X] 0.45362E-03 c Velocity[Y] 0.25138E-02 c Velocity[Z] 0.49667E-29 c Pressure 0.34702E-03 11 0.28150E-07 0.72701E-01 0.11664E-02 c TempK 0.39076E+02 85 0.71777E-03 0.98244E-02 0.33695E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22244 0.19651 4.6843e-006 4.6843e-006 v Velocity[Y] -0.30482 1.0577 0.011189 0.011189 v Velocity[Z] -5.8801e-014 5.1004e-014 -1.0299e-016 -1.0299e-016 v ǁVelocityǁ 0.0011543 1.0577 0.077179 0.077179 v Pressure -1.0005 1.0079 1.1102e-015 1.6697e-015 v TempK 293 305.31 295.38 295.38 v Density 1 1 1 1 v CourantNb 0.42437 8 7.4826 7.4826 v FourierNb 0.12866 4.2961 0.7033 0.7033 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27464 10.195 1.5244 1.5244 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.92 305.6 295.42 295.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73044 11.686 8.1859 8.1859 INSTANT 0.182000000E+02 TIME STEP NUMBER 182 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.18301E-02 0.55649E-01 Friction velocity uk : 0.18301E-02 0.55649E-01 Dimensionless distance yplus : 0.62504E+00 0.19006E+02 Friction thermal sca. tstar : -0.49414E+01 0.21957E+01 Rough dim-less th. sca. tplus : 0.44377E+00 0.13494E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.97138E-04 114 0.25284E+00 0.31423E-02 0.64974E+00 c Velocity[X] 0.44190E-03 c Velocity[Y] 0.27004E-02 c Velocity[Z] 0.41212E-29 c Pressure 0.33377E-03 11 0.27547E-07 0.70017E-01 0.11551E-02 c TempK 0.39155E+02 85 0.53653E-03 0.90578E-02 0.32507E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18199 0.16198 -2.353e-005 -2.353e-005 v Velocity[Y] -0.25417 0.89232 0.011008 0.011008 v Velocity[Z] -5.9905e-014 5.7329e-014 -1.2383e-016 -1.2383e-016 v ǁVelocityǁ 0.00048514 0.8953 0.076983 0.076983 v Pressure -1.0006 1.0068 4.6185e-016 1.0408e-015 v TempK 293.07 305.85 295.39 295.39 v Density 1 1 1 1 v CourantNb 0.46614 8 7.4748 7.4748 v FourierNb 0.10508 4.7257 0.70107 0.70107 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.25694 11.215 1.5209 1.5209 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293 305.31 295.43 295.42 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.71388 12.241 8.1758 8.1758 INSTANT 0.183000000E+02 TIME STEP NUMBER 183 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.78751E-03 0.44805E-01 Friction velocity uk : 0.78751E-03 0.44805E-01 Dimensionless distance yplus : 0.26896E+00 0.15302E+02 Friction thermal sca. tstar : -0.89477E+01 0.15180E+01 Rough dim-less th. sca. tplus : 0.19096E+00 0.10864E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.95571E-04 115 0.24295E+00 0.30236E-02 0.63504E+00 c Velocity[X] 0.46873E-03 c Velocity[Y] 0.25549E-02 c Velocity[Z] 0.56237E-29 c Pressure 0.33885E-03 10 0.30055E-07 0.69415E-01 0.10750E-02 c TempK 0.39149E+02 85 0.63648E-03 0.75173E-02 0.29798E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15884 0.17122 3.7e-006 3.7e-006 v Velocity[Y] -0.24949 0.9301 0.010871 0.010871 v Velocity[Z] -6.0327e-014 5.0603e-014 -1.1787e-016 -1.1787e-016 v ǁVelocityǁ 0.00081947 0.9303 0.076652 0.076652 v Pressure -1.0009 1.0064 -9.9476e-016 -3.9031e-016 v TempK 293.12 305.39 295.4 295.4 v Density 1 1 1 1 v CourantNb 0.62758 8 7.4518 7.4518 v FourierNb 0.11558 4.8538 0.70184 0.70184 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28264 12.336 1.5237 1.5237 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.07 305.85 295.44 295.43 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.2042 12.854 8.1537 8.1537 INSTANT 0.184000000E+02 TIME STEP NUMBER 184 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14211E-02 0.50605E-01 Friction velocity uk : 0.14211E-02 0.50605E-01 Dimensionless distance yplus : 0.48535E+00 0.17283E+02 Friction thermal sca. tstar : -0.14020E+02 0.17987E+01 Rough dim-less th. sca. tplus : 0.34459E+00 0.12271E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94424E-04 115 0.22662E+00 0.29477E-02 0.62469E+00 c Velocity[X] 0.47386E-03 c Velocity[Y] 0.24738E-02 c Velocity[Z] 0.50402E-29 c Pressure 0.32981E-03 11 0.32189E-07 0.64787E-01 0.10531E-02 c TempK 0.39195E+02 84 0.54094E-03 0.71718E-02 0.29702E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17408 0.17962 -4.1844e-006 -4.1844e-006 v Velocity[Y] -0.25251 0.99037 0.010886 0.010886 v Velocity[Z] -5.9825e-014 4.9974e-014 -1.3673e-016 -1.3673e-016 v ǁVelocityǁ 0.00096231 0.99037 0.076723 0.076723 v Pressure -1.0012 1.0067 3.2863e-016 8.8905e-016 v TempK 293.11 306.12 295.42 295.42 v Density 1 1 1 1 v CourantNb 0.27812 8 7.4501 7.4501 v FourierNb 0.12714 5.3196 0.70039 0.70039 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27994 13.57 1.5205 1.5205 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.12 305.39 295.45 295.44 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.699 12.726 8.1505 8.1505 INSTANT 0.185000000E+02 TIME STEP NUMBER 185 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.94946E-03 0.45218E-01 Friction velocity uk : 0.94946E-03 0.45218E-01 Dimensionless distance yplus : 0.32427E+00 0.15443E+02 Friction thermal sca. tstar : -0.44279E+01 0.20612E+01 Rough dim-less th. sca. tplus : 0.23023E+00 0.10965E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.93588E-04 116 0.24033E+00 0.30169E-02 0.63344E+00 c Velocity[X] 0.47893E-03 c Velocity[Y] 0.25379E-02 c Velocity[Z] 0.52955E-29 c Pressure 0.32576E-03 11 0.34229E-07 0.61462E-01 0.11371E-02 c TempK 0.39202E+02 84 0.51437E-03 0.69972E-02 0.27679E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1685 0.18503 1.6611e-006 1.6611e-006 v Velocity[Y] -0.22546 0.88531 0.010846 0.010846 v Velocity[Z] -5.5227e-014 5.2869e-014 -1.4438e-016 -1.4438e-016 v ǁVelocityǁ 0.001005 0.88531 0.076212 0.076212 v Pressure -1.0015 1.0069 1.0658e-016 7.1557e-016 v TempK 293.04 305.85 295.43 295.43 v Density 1 1 1 1 v CourantNb 0.20068 8 7.434 7.434 v FourierNb 0.12606 5.4864 0.69712 0.69712 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26908 14.927 1.5142 1.5142 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.11 306.12 295.47 295.46 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.87188 13.249 8.1311 8.1311 INSTANT 0.186000000E+02 TIME STEP NUMBER 186 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.58722E-03 0.47170E-01 Friction velocity uk : 0.58722E-03 0.47170E-01 Dimensionless distance yplus : 0.20055E+00 0.16110E+02 Friction thermal sca. tstar : -0.72411E+01 0.11750E+01 Rough dim-less th. sca. tplus : 0.14239E+00 0.11438E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.92014E-04 116 0.23186E+00 0.28138E-02 0.60256E+00 c Velocity[X] 0.46226E-03 c Velocity[Y] 0.23515E-02 c Velocity[Z] 0.56620E-29 c Pressure 0.33376E-03 11 0.32749E-07 0.60723E-01 0.10752E-02 c TempK 0.39131E+02 83 0.51051E-03 0.62701E-02 0.25968E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17795 0.19364 -9.1655e-006 -9.1655e-006 v Velocity[Y] -0.2168 0.91477 0.010955 0.010955 v Velocity[Z] -5.3605e-014 6.3497e-014 -1.2273e-016 -1.2273e-016 v ǁVelocityǁ 0.0012791 0.91522 0.075798 0.075798 v Pressure -1.0019 1.0055 -9.77e-017 5.0958e-016 v TempK 292.93 305.55 295.44 295.44 v Density 1 1 1 1 v CourantNb 0.072023 8 7.4114 7.4114 v FourierNb 0.13322 6.035 0.69217 0.69217 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28436 14.428 1.5039 1.5039 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.04 305.85 295.48 295.47 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.70603 13.577 8.1035 8.1035 INSTANT 0.187000000E+02 TIME STEP NUMBER 187 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10458E-02 0.42559E-01 Friction velocity uk : 0.10458E-02 0.42559E-01 Dimensionless distance yplus : 0.35716E+00 0.14535E+02 Friction thermal sca. tstar : -0.32994E+01 0.19775E+01 Rough dim-less th. sca. tplus : 0.25357E+00 0.10320E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.92452E-04 116 0.23030E+00 0.29862E-02 0.64162E+00 c Velocity[X] 0.46925E-03 c Velocity[Y] 0.25170E-02 c Velocity[Z] 0.54360E-29 c Pressure 0.33140E-03 12 0.37268E-07 0.60519E-01 0.11972E-02 c TempK 0.39063E+02 83 0.44839E-03 0.57030E-02 0.25099E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.13957 0.21505 -4.1494e-006 -4.1494e-006 v Velocity[Y] -0.22405 0.93802 0.010864 0.010864 v Velocity[Z] -5.0979e-014 6.8359e-014 -1.3613e-016 -1.3613e-016 v ǁVelocityǁ 0.0006492 0.93803 0.075182 0.075182 v Pressure -1.0024 1.0081 -2.931e-016 3.4694e-016 v TempK 292.82 306.15 295.46 295.46 v Density 1 1 1 1 v CourantNb 0.45826 8 7.3569 7.3569 v FourierNb 0.14195 6.567 0.69267 0.69267 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.303 15.705 1.5054 1.5054 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.93 305.55 295.49 295.48 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.86311 14.178 8.0496 8.0496 INSTANT 0.188000000E+02 TIME STEP NUMBER 188 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.55780E-03 0.47517E-01 Friction velocity uk : 0.55780E-03 0.47517E-01 Dimensionless distance yplus : 0.19050E+00 0.16229E+02 Friction thermal sca. tstar : -0.63200E+01 0.30733E+01 Rough dim-less th. sca. tplus : 0.13525E+00 0.11522E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.93913E-04 116 0.23172E+00 0.30560E-02 0.65655E+00 c Velocity[X] 0.46172E-03 c Velocity[Y] 0.25943E-02 c Velocity[Z] 0.52181E-29 c Pressure 0.32858E-03 15 0.39305E-07 0.63197E-01 0.11615E-02 c TempK 0.39002E+02 82 0.44306E-03 0.56813E-02 0.24079E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16055 0.22431 -1.4797e-005 -1.4797e-005 v Velocity[Y] -0.2525 0.83433 0.010805 0.010805 v Velocity[Z] -4.6705e-014 6.4931e-014 -1.1277e-016 -1.1277e-016 v ǁVelocityǁ 0.00074053 0.83434 0.074716 0.074716 v Pressure -1.0037 1.0065 -3.4639e-016 1.9516e-016 v TempK 292.77 306.39 295.47 295.47 v Density 1 1 1 1 v CourantNb 0.28281 8 7.345 7.345 v FourierNb 0.14801 4.5668 0.69518 0.69518 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31594 12.537 1.511 1.511 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.82 306.15 295.51 295.5 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.49325 12.458 8.0402 8.0402 INSTANT 0.189000000E+02 TIME STEP NUMBER 189 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26557E-03 0.42352E-01 Friction velocity uk : 0.26557E-03 0.42352E-01 Dimensionless distance yplus : 0.90700E-01 0.14464E+02 Friction thermal sca. tstar : -0.86664E+01 0.19548E+01 Rough dim-less th. sca. tplus : 0.64396E-01 0.10270E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89257E-04 116 0.22959E+00 0.27040E-02 0.60175E+00 c Velocity[X] 0.45346E-03 c Velocity[Y] 0.22505E-02 c Velocity[Z] 0.53471E-29 c Pressure 0.32432E-03 11 0.40054E-07 0.62036E-01 0.12426E-02 c TempK 0.38803E+02 82 0.40844E-03 0.76792E-02 0.25377E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23369 0.23909 -2.3504e-006 -2.3504e-006 v Velocity[Y] -0.23437 0.84677 0.011137 0.011137 v Velocity[Z] -5.0808e-014 5.2127e-014 -1.2081e-016 -1.2081e-016 v ǁVelocityǁ 0.00027712 0.84804 0.074405 0.074405 v Pressure -1.0042 1.0073 -1.5543e-015 -9.541e-016 v TempK 292.78 306.4 295.49 295.49 v Density 1 1 1 1 v CourantNb 0.39457 8 7.3128 7.3128 v FourierNb 0.14159 4.7906 0.70234 0.70234 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30224 13.634 1.5278 1.5278 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.77 306.39 295.52 295.51 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0447 12.791 8.0152 8.0152 INSTANT 0.190000000E+02 TIME STEP NUMBER 190 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.59304E-03 0.47402E-01 Friction velocity uk : 0.59304E-03 0.47402E-01 Dimensionless distance yplus : 0.20254E+00 0.16189E+02 Friction thermal sca. tstar : -0.98941E+01 0.17577E+01 Rough dim-less th. sca. tplus : 0.14380E+00 0.11494E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94118E-04 116 0.23085E+00 0.28358E-02 0.61396E+00 c Velocity[X] 0.50722E-03 c Velocity[Y] 0.23286E-02 c Velocity[Z] 0.53566E-29 c Pressure 0.34437E-03 11 0.41257E-07 0.66158E-01 0.13719E-02 c TempK 0.38579E+02 86 0.40788E-03 0.76595E-02 0.25492E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18801 0.24175 -7.6479e-006 -7.6479e-006 v Velocity[Y] -0.32838 0.94391 0.011119 0.011119 v Velocity[Z] -5.9385e-014 5.228e-014 -1.2875e-016 -1.2875e-016 v ǁVelocityǁ 0.001084 0.94436 0.074566 0.074566 v Pressure -1.0041 1.0065 -1.652e-015 -1.0083e-015 v TempK 292.81 306.28 295.5 295.5 v Density 1 1 1 1 v CourantNb 0.098897 8 7.2939 7.2939 v FourierNb 0.1383 3.8883 0.70768 0.70768 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29522 9.383 1.5372 1.5372 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.78 306.4 295.54 295.53 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1313 11.888 8.0016 8.0016 INSTANT 0.191000000E+02 TIME STEP NUMBER 191 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.44258E-03 0.43747E-01 Friction velocity uk : 0.44258E-03 0.43747E-01 Dimensionless distance yplus : 0.15116E+00 0.14941E+02 Friction thermal sca. tstar : -0.22631E+02 0.17234E+01 Rough dim-less th. sca. tplus : 0.10732E+00 0.10608E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.93052E-04 116 0.25122E+00 0.28671E-02 0.63461E+00 c Velocity[X] 0.48507E-03 c Velocity[Y] 0.23820E-02 c Velocity[Z] 0.53287E-29 c Pressure 0.32483E-03 11 0.38074E-07 0.64012E-01 0.14062E-02 c TempK 0.38464E+02 82 0.55341E-03 0.89642E-02 0.28575E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19901 0.24647 -9.6715e-007 -9.6715e-007 v Velocity[Y] -0.37469 1.0046 0.01096 0.01096 v Velocity[Z] -5.5669e-014 4.6622e-014 -1.3006e-016 -1.3006e-016 v ǁVelocityǁ 0.00045349 1.0113 0.073664 0.073664 v Pressure -1.0053 1.0066 -7.4607e-016 -1.0842e-016 v TempK 292.83 305.85 295.51 295.51 v Density 1 1 1 1 v CourantNb 0.31093 8 7.2945 7.2945 v FourierNb 0.12824 3.6265 0.71794 0.71794 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.27749 10.321 1.5607 1.5607 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.81 306.28 295.55 295.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0702 11.377 8.0124 8.0124 INSTANT 0.192000000E+02 TIME STEP NUMBER 192 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.52320E-04 0.49904E-01 Friction velocity uk : 0.52320E-04 0.49904E-01 Dimensionless distance yplus : 0.17869E-01 0.17044E+02 Friction thermal sca. tstar : -0.13011E+02 0.17753E+01 Rough dim-less th. sca. tplus : 0.12687E-01 0.12101E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.92696E-04 116 0.24242E+00 0.26766E-02 0.58479E+00 c Velocity[X] 0.47437E-03 c Velocity[Y] 0.22022E-02 c Velocity[Z] 0.54278E-29 c Pressure 0.34444E-03 11 0.37641E-07 0.65419E-01 0.14325E-02 c TempK 0.38062E+02 83 0.47654E-03 0.11006E-01 0.31523E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19034 0.26004 -9.3738e-006 -9.3738e-006 v Velocity[Y] -0.3156 0.93592 0.011117 0.011117 v Velocity[Z] -5.9127e-014 4.8486e-014 -1.3051e-016 -1.3051e-016 v ǁVelocityǁ 0.00046565 0.93613 0.073738 0.073738 v Pressure -1.0055 1.01 -7.2831e-016 -1.0842e-016 v TempK 292.82 305.14 295.53 295.53 v Density 1 1 1 1 v CourantNb 0.33945 8 7.2595 7.2595 v FourierNb 0.12803 3.9891 0.73142 0.73142 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2913 11.353 1.5903 1.5903 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.83 305.85 295.56 295.55 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.80185 11.521 7.9909 7.9909 INSTANT 0.193000000E+02 TIME STEP NUMBER 193 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14157E-03 0.44576E-01 Friction velocity uk : 0.14157E-03 0.44576E-01 Dimensionless distance yplus : 0.48351E-01 0.15224E+02 Friction thermal sca. tstar : -0.45016E+02 0.24016E+01 Rough dim-less th. sca. tplus : 0.34328E-01 0.10809E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94455E-04 116 0.26807E+00 0.31786E-02 0.66688E+00 c Velocity[X] 0.49360E-03 c Velocity[Y] 0.26850E-02 c Velocity[Z] 0.48914E-29 c Pressure 0.34534E-03 11 0.31449E-07 0.63929E-01 0.13647E-02 c TempK 0.37826E+02 84 0.54775E-03 0.12889E-01 0.36576E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16907 0.24648 -1.4723e-005 -1.4723e-005 v Velocity[Y] -0.27407 0.98081 0.010976 0.010976 v Velocity[Z] -5.6146e-014 4.7247e-014 -1.4708e-016 -1.4708e-016 v ǁVelocityǁ 0.0004691 0.98771 0.073658 0.073658 v Pressure -1.006 1.0066 -1.9096e-015 -1.301e-015 v TempK 292.82 304.77 295.55 295.55 v Density 1 1 1 1 v CourantNb 0.18326 8 7.2952 7.2952 v FourierNb 0.11904 4.1912 0.74535 0.74535 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29239 11.929 1.6213 1.6213 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.82 305.14 295.58 295.57 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.3813 12.191 8.0405 8.0405 INSTANT 0.194000000E+02 TIME STEP NUMBER 194 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10118E-02 0.48934E-01 Friction velocity uk : 0.10118E-02 0.48934E-01 Dimensionless distance yplus : 0.34555E+00 0.16712E+02 Friction thermal sca. tstar : -0.51519E+01 0.98937E+00 Rough dim-less th. sca. tplus : 0.24533E+00 0.11866E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.92837E-04 115 0.25431E+00 0.29549E-02 0.64039E+00 c Velocity[X] 0.44818E-03 c Velocity[Y] 0.25067E-02 c Velocity[Z] 0.47450E-29 c Pressure 0.31803E-03 10 0.30978E-07 0.58478E-01 0.13390E-02 c TempK 0.37591E+02 85 0.54977E-03 0.14954E-01 0.39100E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20883 0.25896 -2.0249e-005 -2.0249e-005 v Velocity[Y] -0.27127 1.0627 0.010852 0.010852 v Velocity[Z] -5.7913e-014 5.206e-014 -1.5046e-016 -1.5046e-016 v ǁVelocityǁ 0.00035826 1.0639 0.073476 0.073476 v Pressure -1.0056 1.0054 -1.279e-015 -6.6136e-016 v TempK 292.84 304.41 295.57 295.57 v Density 1 1 1 1 v CourantNb 0.22615 8 7.3351 7.3351 v FourierNb 0.10935 4.26 0.75349 0.75349 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.26485 12.124 1.6392 1.6392 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.82 304.77 295.6 295.59 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.65396 11.9 8.0886 8.0886 INSTANT 0.195000000E+02 TIME STEP NUMBER 195 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.98679E-03 0.43357E-01 Friction velocity uk : 0.98679E-03 0.43357E-01 Dimensionless distance yplus : 0.33702E+00 0.14808E+02 Friction thermal sca. tstar : -0.67812E+01 0.14218E+01 Rough dim-less th. sca. tplus : 0.23928E+00 0.10513E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.94353E-04 115 0.28089E+00 0.30376E-02 0.67836E+00 c Velocity[X] 0.45418E-03 c Velocity[Y] 0.25835E-02 c Velocity[Z] 0.54299E-29 c Pressure 0.33188E-03 11 0.31880E-07 0.60372E-01 0.12397E-02 c TempK 0.37307E+02 87 0.61018E-03 0.15374E-01 0.39981E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15925 0.25129 -6.8195e-006 -6.8195e-006 v Velocity[Y] -0.22302 0.95749 0.010976 0.010976 v Velocity[Z] -6.5058e-014 5.2772e-014 -1.5538e-016 -1.5538e-016 v ǁVelocityǁ 0.00025998 0.95787 0.073548 0.073548 v Pressure -1.0048 1.0072 -9.8588e-016 -3.5779e-016 v TempK 292.91 303.92 295.58 295.58 v Density 1 1 1 1 v CourantNb 0.56381 8 7.3462 7.3462 v FourierNb 0.11238 4.686 0.75673 0.75673 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.2632 13.337 1.6471 1.6471 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.84 304.41 295.62 295.61 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.86622 11.556 8.1029 8.1029 INSTANT 0.196000000E+02 TIME STEP NUMBER 196 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.42165E-03 0.47442E-01 Friction velocity uk : 0.42165E-03 0.47442E-01 Dimensionless distance yplus : 0.14401E+00 0.16203E+02 Friction thermal sca. tstar : -0.67056E+01 0.70726E+00 Rough dim-less th. sca. tplus : 0.10224E+00 0.11504E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.89257E-04 115 0.24909E+00 0.27821E-02 0.62346E+00 c Velocity[X] 0.43143E-03 c Velocity[Y] 0.23507E-02 c Velocity[Z] 0.49636E-29 c Pressure 0.32422E-03 11 0.29823E-07 0.58445E-01 0.10980E-02 c TempK 0.36964E+02 88 0.52694E-03 0.16479E-01 0.42791E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1703 0.23232 -4.4256e-006 -4.4256e-006 v Velocity[Y] -0.25751 0.89513 0.01079 0.01079 v Velocity[Z] -6.706e-014 5.4252e-014 -1.3973e-016 -1.3973e-016 v ǁVelocityǁ 0.00045366 0.90228 0.073146 0.073146 v Pressure -1.0039 1.0067 -1.652e-015 -1.0625e-015 v TempK 292.98 303.42 295.6 295.6 v Density 1 1 1 1 v CourantNb 0.02583 8 7.3622 7.3622 v FourierNb 0.12361 5.1547 0.76053 0.76053 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28952 14.671 1.656 1.656 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.91 303.92 295.63 295.62 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.68042 11.764 8.1227 8.1227 INSTANT 0.197000000E+02 TIME STEP NUMBER 197 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.74659E-03 0.43682E-01 Friction velocity uk : 0.74659E-03 0.43682E-01 Dimensionless distance yplus : 0.25498E+00 0.14919E+02 Friction thermal sca. tstar : -0.40844E+01 0.15752E+00 Rough dim-less th. sca. tplus : 0.18103E+00 0.10592E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.84689E-04 115 0.25540E+00 0.26772E-02 0.60547E+00 c Velocity[X] 0.43229E-03 c Velocity[Y] 0.22449E-02 c Velocity[Z] 0.49215E-29 c Pressure 0.31815E-03 11 0.30666E-07 0.56667E-01 0.11327E-02 c TempK 0.36573E+02 89 0.56596E-03 0.17241E-01 0.42751E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1634 0.23306 8.9011e-006 8.9011e-006 v Velocity[Y] -0.27092 0.81545 0.010946 0.010946 v Velocity[Z] -6.4741e-014 5.7864e-014 -1.4118e-016 -1.4118e-016 v ǁVelocityǁ 0.0010229 0.81567 0.073236 0.073236 v Pressure -1.0037 1.0069 -6.6613e-016 -1.5179e-016 v TempK 293.03 302.67 295.61 295.61 v Density 1 1 1 1 v CourantNb 0.26188 8 7.3244 7.3244 v FourierNb 0.13598 5.6701 0.77189 0.77189 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31848 16.138 1.6812 1.6812 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.98 303.42 295.64 295.64 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.2786 13.29 8.0963 8.0963 INSTANT 0.198000000E+02 TIME STEP NUMBER 198 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.59829E-03 0.44664E-01 Friction velocity uk : 0.59829E-03 0.44664E-01 Dimensionless distance yplus : 0.20434E+00 0.15254E+02 Friction thermal sca. tstar : -0.53195E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.14507E+00 0.10830E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.84092E-04 115 0.26549E+00 0.27515E-02 0.61184E+00 c Velocity[X] 0.45220E-03 c Velocity[Y] 0.22993E-02 c Velocity[Z] 0.52072E-29 c Pressure 0.33248E-03 11 0.27971E-07 0.57463E-01 0.10815E-02 c TempK 0.36200E+02 90 0.51632E-03 0.14597E-01 0.41212E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22183 0.25282 -4.933e-007 -4.933e-007 v Velocity[Y] -0.26308 0.95201 0.010923 0.010923 v Velocity[Z] -6.2127e-014 5.5695e-014 -1.1617e-016 -1.1617e-016 v ǁVelocityǁ 0.00076416 0.95236 0.073133 0.073133 v Pressure -1.0036 1.0061 -8.0824e-016 -1.0842e-016 v TempK 293.02 303 295.61 295.61 v Density 1 1 1 1 v CourantNb 0.61981 8 7.3341 7.3341 v FourierNb 0.14957 5.1605 0.77954 0.77954 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33545 14.687 1.6976 1.6976 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.03 303.15 295.65 295.64 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0475 12.047 8.1137 8.1137 INSTANT 0.199000000E+02 TIME STEP NUMBER 199 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.34276E-03 0.42107E-01 Friction velocity uk : 0.34276E-03 0.42107E-01 Dimensionless distance yplus : 0.11706E+00 0.14381E+02 Friction thermal sca. tstar : -0.68344E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.83112E-01 0.10210E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82860E-04 116 0.27923E+00 0.29921E-02 0.64834E+00 c Velocity[X] 0.48165E-03 c Velocity[Y] 0.25104E-02 c Velocity[Z] 0.48740E-29 c Pressure 0.32362E-03 11 0.27494E-07 0.53517E-01 0.12035E-02 c TempK 0.35948E+02 90 0.48222E-03 0.14267E-01 0.40013E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21876 0.2701 9.4178e-006 9.4178e-006 v Velocity[Y] -0.32863 0.85645 0.010903 0.010903 v Velocity[Z] -6.1101e-014 6.5933e-014 -1.3312e-016 -1.3312e-016 v ǁVelocityǁ 0.0002268 0.85648 0.073173 0.073173 v Pressure -1.0036 1.0074 3.3751e-016 9.4326e-016 v TempK 293.02 303.4 295.62 295.62 v Density 1 1 1 1 v CourantNb 0.43223 8 7.3048 7.3048 v FourierNb 0.16453 4.9838 0.79034 0.79034 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35124 14.184 1.7206 1.7206 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.02 303.15 295.66 295.65 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.2275 12.317 8.0951 8.0951 INSTANT 0.200000000E+02 TIME STEP NUMBER 200 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.16269E-03 0.44522E-01 Friction velocity uk : 0.16269E-03 0.44522E-01 Dimensionless distance yplus : 0.55563E-01 0.15205E+02 Friction thermal sca. tstar : -0.95130E+01 0.49269E+00 Rough dim-less th. sca. tplus : 0.39449E-01 0.10796E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83689E-04 116 0.28631E+00 0.28618E-02 0.64170E+00 c Velocity[X] 0.43812E-03 c Velocity[Y] 0.24237E-02 c Velocity[Z] 0.51165E-29 c Pressure 0.32823E-03 11 0.25015E-07 0.52009E-01 0.13239E-02 c TempK 0.35795E+02 91 0.41527E-03 0.12796E-01 0.38357E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20497 0.26764 -1.5879e-005 -1.5879e-005 v Velocity[Y] -0.32891 0.87914 0.010765 0.010765 v Velocity[Z] -5.9688e-014 5.4093e-014 -1.361e-016 -1.361e-016 v ǁVelocityǁ 0.00050379 0.8794 0.072838 0.072838 v Pressure -1.0037 1.007 -5.0626e-016 6.5052e-017 v TempK 293.03 303.74 295.63 295.63 v Density 1 1 1 1 v CourantNb 0.40452 8 7.3382 7.3382 v FourierNb 0.13108 5.1687 0.79887 0.79887 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3498 14.71 1.7385 1.7385 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.02 303.4 295.67 295.66 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69157 13.169 8.137 8.137 INSTANT 0.201000000E+02 TIME STEP NUMBER 201 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.64711E-03 0.38020E-01 Friction velocity uk : 0.64711E-03 0.38020E-01 Dimensionless distance yplus : 0.22101E+00 0.12985E+02 Friction thermal sca. tstar : -0.88858E+01 0.10544E+01 Rough dim-less th. sca. tplus : 0.15691E+00 0.92190E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79900E-04 117 0.28302E+00 0.27396E-02 0.61243E+00 c Velocity[X] 0.43903E-03 c Velocity[Y] 0.23006E-02 c Velocity[Z] 0.51654E-29 c Pressure 0.33186E-03 11 0.22763E-07 0.50838E-01 0.11902E-02 c TempK 0.35458E+02 91 0.42267E-03 0.11980E-01 0.36265E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20409 0.2538 -8.9616e-006 -8.9616e-006 v Velocity[Y] -0.28691 0.91803 0.010916 0.010916 v Velocity[Z] -6.0402e-014 5.6828e-014 -1.3727e-016 -1.3727e-016 v ǁVelocityǁ 0.00018903 0.91966 0.072889 0.072889 v Pressure -1.0035 1.0056 -4.5297e-016 1.4095e-016 v TempK 293.05 303.94 295.64 295.64 v Density 1 1 1 1 v CourantNb 0.326 8 7.3032 7.3032 v FourierNb 0.12729 5.2235 0.8149 0.8149 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30534 14.867 1.7734 1.7734 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.03 303.74 295.68 295.67 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.63008 12.369 8.1182 8.1182 INSTANT 0.202000000E+02 TIME STEP NUMBER 202 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.34740E-03 0.45946E-01 Friction velocity uk : 0.34740E-03 0.45946E-01 Dimensionless distance yplus : 0.11865E+00 0.15692E+02 Friction thermal sca. tstar : -0.41917E+01 0.96180E+00 Rough dim-less th. sca. tplus : 0.84237E-01 0.11141E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80212E-04 118 0.26199E+00 0.29338E-02 0.64316E+00 c Velocity[X] 0.52054E-03 c Velocity[Y] 0.24133E-02 c Velocity[Z] 0.52799E-29 c Pressure 0.33888E-03 11 0.30399E-07 0.52371E-01 0.11589E-02 c TempK 0.35279E+02 91 0.36180E-03 0.10868E-01 0.35518E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20497 0.23548 -1.2023e-005 -1.2023e-005 v Velocity[Y] -0.25925 1.0599 0.010652 0.010652 v Velocity[Z] -5.4613e-014 5.7719e-014 -1.2112e-016 -1.2112e-016 v ǁVelocityǁ 0.00087765 1.0641 0.072617 0.072617 v Pressure -1.0033 1.0081 -6.6613e-016 -6.5052e-017 v TempK 293.06 304.19 295.64 295.64 v Density 1 1 1 1 v CourantNb 0.30588 8 7.4076 7.4076 v FourierNb 0.13884 5.7459 0.80292 0.80292 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30686 16.353 1.7477 1.7477 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.05 303.94 295.69 295.68 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.78966 12.444 8.2105 8.2105 INSTANT 0.203000000E+02 TIME STEP NUMBER 203 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.74615E-03 0.44640E-01 Friction velocity uk : 0.74615E-03 0.44640E-01 Dimensionless distance yplus : 0.25483E+00 0.15246E+02 Friction thermal sca. tstar : -0.46231E+01 0.16205E+01 Rough dim-less th. sca. tplus : 0.18093E+00 0.10824E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79425E-04 119 0.27103E+00 0.31130E-02 0.68101E+00 c Velocity[X] 0.51932E-03 c Velocity[Y] 0.25937E-02 c Velocity[Z] 0.50645E-29 c Pressure 0.32622E-03 11 0.25970E-07 0.53391E-01 0.11575E-02 c TempK 0.35255E+02 91 0.41035E-03 0.96460E-02 0.32979E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18764 0.21139 -5.2277e-006 -5.2277e-006 v Velocity[Y] -0.26473 0.90238 0.010612 0.010612 v Velocity[Z] -5.4268e-014 5.861e-014 -1.3032e-016 -1.3032e-016 v ǁVelocityǁ 0.00055971 0.90557 0.072471 0.072471 v Pressure -1.0028 1.0081 3.5527e-017 6.8305e-016 v TempK 293.05 304.54 295.65 295.65 v Density 1 1 1 1 v CourantNb 0.43437 8 7.4044 7.4044 v FourierNb 0.14427 5.0563 0.78576 0.78576 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30796 13.007 1.7117 1.7117 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.06 304.19 295.69 295.68 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.96489 12.176 8.1902 8.1902 INSTANT 0.204000000E+02 TIME STEP NUMBER 204 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.16693E-03 0.42764E-01 Friction velocity uk : 0.16693E-03 0.42764E-01 Dimensionless distance yplus : 0.57012E-01 0.14605E+02 Friction thermal sca. tstar : -0.42920E+01 0.24535E+01 Rough dim-less th. sca. tplus : 0.40478E-01 0.10369E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.78853E-04 118 0.24894E+00 0.30663E-02 0.66404E+00 c Velocity[X] 0.53693E-03 c Velocity[Y] 0.25294E-02 c Velocity[Z] 0.55526E-29 c Pressure 0.33407E-03 11 0.29568E-07 0.55281E-01 0.11815E-02 c TempK 0.35321E+02 90 0.35830E-03 0.84595E-02 0.31712E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18233 0.18036 -3.5511e-005 -3.5511e-005 v Velocity[Y] -0.24728 0.97236 0.010805 0.010805 v Velocity[Z] -4.4867e-014 5.8004e-014 -1.2643e-016 -1.2643e-016 v ǁVelocityǁ 0.00022984 0.97818 0.072928 0.072928 v Pressure -1.0024 1.0083 -3.1974e-016 2.3852e-016 v TempK 293.03 304.66 295.66 295.66 v Density 1 1 1 1 v CourantNb 0.33127 8 7.4244 7.4244 v FourierNb 0.14295 5.1448 0.78111 0.78111 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30513 14.307 1.7023 1.7023 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.05 304.54 295.7 295.69 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60576 12.551 8.2055 8.2055 INSTANT 0.205000000E+02 TIME STEP NUMBER 205 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.66749E-03 0.45164E-01 Friction velocity uk : 0.66749E-03 0.45164E-01 Dimensionless distance yplus : 0.22797E+00 0.15425E+02 Friction thermal sca. tstar : -0.62244E+01 0.14103E+01 Rough dim-less th. sca. tplus : 0.16185E+00 0.10951E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.78883E-04 118 0.26206E+00 0.31159E-02 0.68692E+00 c Velocity[X] 0.54330E-03 c Velocity[Y] 0.25726E-02 c Velocity[Z] 0.57674E-29 c Pressure 0.32333E-03 10 0.26722E-07 0.54154E-01 0.11462E-02 c TempK 0.35432E+02 90 0.27390E-03 0.77508E-02 0.29720E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19425 0.17116 -1.4192e-005 -1.4192e-005 v Velocity[Y] -0.24604 0.86571 0.010708 0.010708 v Velocity[Z] -5.8606e-014 5.4377e-014 -1.3323e-016 -1.3323e-016 v ǁVelocityǁ 0.00083841 0.8733 0.072423 0.072423 v Pressure -1.0022 1.0096 2.6645e-016 8.0231e-016 v TempK 293.01 304.56 295.66 295.66 v Density 1 1 1 1 v CourantNb 0.5033 8 7.4493 7.4493 v FourierNb 0.14195 5.5297 0.77311 0.77311 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30301 15.738 1.687 1.687 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.03 304.66 295.7 295.69 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72207 11.992 8.2224 8.2224 INSTANT 0.206000000E+02 TIME STEP NUMBER 206 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.56664E-03 0.44077E-01 Friction velocity uk : 0.56664E-03 0.44077E-01 Dimensionless distance yplus : 0.19352E+00 0.15054E+02 Friction thermal sca. tstar : -0.15018E+02 0.96705E+00 Rough dim-less th. sca. tplus : 0.13740E+00 0.10688E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74524E-04 118 0.25696E+00 0.27381E-02 0.62216E+00 c Velocity[X] 0.51275E-03 c Velocity[Y] 0.22254E-02 c Velocity[Z] 0.60784E-29 c Pressure 0.33174E-03 11 0.30213E-07 0.53713E-01 0.10424E-02 c TempK 0.35211E+02 89 0.29521E-03 0.75251E-02 0.29906E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16661 0.15842 -2.3729e-005 -2.3729e-005 v Velocity[Y] -0.24587 0.9754 0.010843 0.010843 v Velocity[Z] -5.756e-014 5.2975e-014 -1.0656e-016 -1.0656e-016 v ǁVelocityǁ 0.00047358 0.98071 0.07241 0.07241 v Pressure -1.0021 1.0089 -3.7303e-016 1.5179e-016 v TempK 292.99 304.7 295.67 295.67 v Density 1 1 1 1 v CourantNb 0.39866 8 7.4526 7.4526 v FourierNb 0.14519 6.0827 0.77412 0.77412 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.30993 17.312 1.6893 1.6893 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.01 304.56 295.71 295.7 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.64816 13.315 8.2267 8.2267 INSTANT 0.207000000E+02 TIME STEP NUMBER 207 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.31824E-03 0.45854E-01 Friction velocity uk : 0.31824E-03 0.45854E-01 Dimensionless distance yplus : 0.10869E+00 0.15660E+02 Friction thermal sca. tstar : -0.17379E+02 0.19629E+01 Rough dim-less th. sca. tplus : 0.77168E-01 0.11119E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75712E-04 118 0.26258E+00 0.29304E-02 0.64322E+00 c Velocity[X] 0.52066E-03 c Velocity[Y] 0.24097E-02 c Velocity[Z] 0.52159E-29 c Pressure 0.33059E-03 11 0.25266E-07 0.51002E-01 0.10417E-02 c TempK 0.35053E+02 88 0.32529E-03 0.78769E-02 0.29366E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16888 0.1752 -1.4389e-005 -1.4389e-005 v Velocity[Y] -0.24731 0.82072 0.010839 0.010839 v Velocity[Z] -6.8241e-014 5.2623e-014 -1.0716e-016 -1.0716e-016 v ǁVelocityǁ 0.00050522 0.82691 0.072393 0.072393 v Pressure -1.0018 1.008 1.7764e-017 5.5294e-016 v TempK 292.97 304.93 295.68 295.68 v Density 1 1 1 1 v CourantNb 0.38943 8 7.4857 7.4857 v FourierNb 0.14719 6.6909 0.76846 0.76846 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31418 19.043 1.6747 1.6747 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.99 304.7 295.71 295.7 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.106 13.453 8.2542 8.2542 INSTANT 0.208000000E+02 TIME STEP NUMBER 208 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.31703E-03 0.46827E-01 Friction velocity uk : 0.31703E-03 0.46827E-01 Dimensionless distance yplus : 0.10828E+00 0.15993E+02 Friction thermal sca. tstar : -0.36346E+01 0.20268E+01 Rough dim-less th. sca. tplus : 0.76874E-01 0.11355E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73449E-04 116 0.25980E+00 0.29946E-02 0.65442E+00 c Velocity[X] 0.53077E-03 c Velocity[Y] 0.24639E-02 c Velocity[Z] 0.56484E-29 c Pressure 0.31732E-03 12 0.29667E-07 0.48917E-01 0.10791E-02 c TempK 0.34977E+02 86 0.30291E-03 0.68791E-02 0.28416E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17542 0.18135 -2.0024e-005 -2.0024e-005 v Velocity[Y] -0.25065 0.92382 0.010811 0.010811 v Velocity[Z] -5.2325e-014 5.6501e-014 -9.736e-017 -9.736e-017 v ǁVelocityǁ 0.0010139 0.9308 0.071929 0.071929 v Pressure -1.0015 1.0066 -4.2633e-016 2.8189e-016 v TempK 292.97 304.84 295.68 295.68 v Density 1 1 1 1 v CourantNb 0.38019 8 7.5023 7.5023 v FourierNb 0.14739 5.5207 0.76527 0.76527 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31461 15.712 1.6645 1.6645 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.97 304.93 295.72 295.71 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69791 13.074 8.2675 8.2675 INSTANT 0.209000000E+02 TIME STEP NUMBER 209 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.90871E-03 0.44849E-01 Friction velocity uk : 0.90871E-03 0.44849E-01 Dimensionless distance yplus : 0.31035E+00 0.15317E+02 Friction thermal sca. tstar : -0.86824E+01 0.13746E+01 Rough dim-less th. sca. tplus : 0.22035E+00 0.10875E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73711E-04 116 0.27078E+00 0.31889E-02 0.69196E+00 c Velocity[X] 0.51611E-03 c Velocity[Y] 0.26728E-02 c Velocity[Z] 0.50791E-29 c Pressure 0.31799E-03 11 0.25465E-07 0.46461E-01 0.97038E-03 c TempK 0.34955E+02 86 0.37138E-03 0.77890E-02 0.29129E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17833 0.13961 1.1266e-005 1.1266e-005 v Velocity[Y] -0.25819 0.82905 0.010709 0.010709 v Velocity[Z] -5.9961e-014 6.2052e-014 -9.7492e-017 -9.7492e-017 v ǁVelocityǁ 0.0002003 0.82933 0.07176 0.07176 v Pressure -1.0014 1.0059 -7.2831e-016 -3.2526e-017 v TempK 292.99 304.59 295.7 295.7 v Density 1 1 1 1 v CourantNb 0.22141 8 7.4933 7.4933 v FourierNb 0.14705 5.2633 0.76967 0.76967 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31389 14.016 1.674 1.674 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.97 304.84 295.73 295.72 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.488 12.925 8.2629 8.2629 INSTANT 0.210000000E+02 TIME STEP NUMBER 210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.73250E-03 0.44268E-01 Friction velocity uk : 0.73250E-03 0.44268E-01 Dimensionless distance yplus : 0.25017E+00 0.15119E+02 Friction thermal sca. tstar : -0.61538E+01 0.92785E+00 Rough dim-less th. sca. tplus : 0.17762E+00 0.10734E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74059E-04 115 0.28010E+00 0.30575E-02 0.68514E+00 c Velocity[X] 0.50627E-03 c Velocity[Y] 0.25512E-02 c Velocity[Z] 0.57403E-29 c Pressure 0.31502E-03 11 0.25156E-07 0.45606E-01 0.10205E-02 c TempK 0.35090E+02 83 0.33987E-03 0.66699E-02 0.27367E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16502 0.16242 -2.3533e-005 -2.3533e-005 v Velocity[Y] -0.26881 0.84855 0.010746 0.010746 v Velocity[Z] -5.8531e-014 6.2996e-014 -1.223e-016 -1.223e-016 v ǁVelocityǁ 0.00048825 0.8539 0.07118 0.07118 v Pressure -1.0014 1.0065 -2.025e-015 -1.3986e-015 v TempK 293.03 304.35 295.7 295.7 v Density 1 1 1 1 v CourantNb 0.40918 8 7.488 7.488 v FourierNb 0.14675 5.7896 0.76877 0.76877 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31325 13.056 1.6719 1.6719 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.99 304.59 295.74 295.73 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67777 12.786 8.2568 8.2568 INSTANT 0.211000000E+02 TIME STEP NUMBER 211 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13404E-03 0.42071E-01 Friction velocity uk : 0.13404E-03 0.42071E-01 Dimensionless distance yplus : 0.45779E-01 0.14369E+02 Friction thermal sca. tstar : -0.58963E+01 0.11411E+01 Rough dim-less th. sca. tplus : 0.32502E-01 0.10201E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72379E-04 115 0.27964E+00 0.28760E-02 0.65617E+00 c Velocity[X] 0.51030E-03 c Velocity[Y] 0.23657E-02 c Velocity[Z] 0.49491E-29 c Pressure 0.33726E-03 12 0.24912E-07 0.48733E-01 0.10974E-02 c TempK 0.34939E+02 82 0.32736E-03 0.73408E-02 0.27414E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15591 0.20313 -6.5143e-006 -6.5143e-006 v Velocity[Y] -0.27244 0.89565 0.010913 0.010913 v Velocity[Z] -6.3038e-014 6.7668e-014 -1.1403e-016 -1.1403e-016 v ǁVelocityǁ 0.00037058 0.89938 0.070841 0.070841 v Pressure -1.0014 1.0062 3.7303e-016 9.3241e-016 v TempK 293.09 304.41 295.71 295.71 v Density 1 1 1 1 v CourantNb 0.10765 8 7.485 7.485 v FourierNb 0.14663 5.5514 0.77175 0.77175 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.313 12.78 1.6777 1.6777 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.03 304.35 295.75 295.74 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.5139 13.551 8.2567 8.2567 INSTANT 0.212000000E+02 TIME STEP NUMBER 212 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.35959E-03 0.45466E-01 Friction velocity uk : 0.35959E-03 0.45466E-01 Dimensionless distance yplus : 0.12281E+00 0.15528E+02 Friction thermal sca. tstar : -0.10397E+02 0.17347E+01 Rough dim-less th. sca. tplus : 0.87193E-01 0.11025E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72502E-04 115 0.27148E+00 0.30514E-02 0.68544E+00 c Velocity[X] 0.53180E-03 c Velocity[Y] 0.25196E-02 c Velocity[Z] 0.49078E-29 c Pressure 0.33157E-03 10 0.22614E-07 0.47606E-01 0.10779E-02 c TempK 0.34705E+02 81 0.30959E-03 0.62480E-02 0.25860E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17702 0.19188 -6.1814e-006 -6.1814e-006 v Velocity[Y] -0.26228 0.84992 0.0107 0.0107 v Velocity[Z] -6.1004e-014 5.378e-014 -1.1231e-016 -1.1231e-016 v ǁVelocityǁ 0.0011742 0.86497 0.070432 0.070432 v Pressure -1.0013 1.007 -5.3291e-017 4.9873e-016 v TempK 293.15 304.41 295.71 295.71 v Density 1 1 1 1 v CourantNb 0.37863 8 7.4824 7.4824 v FourierNb 0.15275 5.7568 0.77475 0.77475 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32605 14.058 1.6828 1.6828 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.09 304.41 295.75 295.74 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.76447 12.942 8.2572 8.2572 INSTANT 0.213000000E+02 TIME STEP NUMBER 213 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.65751E-03 0.46407E-01 Friction velocity uk : 0.65751E-03 0.46407E-01 Dimensionless distance yplus : 0.22456E+00 0.15849E+02 Friction thermal sca. tstar : -0.61897E+01 0.31413E+01 Rough dim-less th. sca. tplus : 0.15943E+00 0.11253E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71132E-04 116 0.28160E+00 0.28121E-02 0.65909E+00 c Velocity[X] 0.49338E-03 c Velocity[Y] 0.23188E-02 c Velocity[Z] 0.45723E-29 c Pressure 0.32194E-03 10 0.21911E-07 0.46022E-01 0.10536E-02 c TempK 0.34396E+02 82 0.35669E-03 0.50779E-02 0.22797E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18178 0.18322 3.8419e-005 3.8419e-005 v Velocity[Y] -0.24124 0.83506 0.010733 0.010733 v Velocity[Z] -6.4236e-014 5.3484e-014 -1.0999e-016 -1.0999e-016 v ǁVelocityǁ 0.00065111 0.83506 0.069412 0.069412 v Pressure -1.0014 1.0077 3.5527e-017 6.8305e-016 v TempK 293.19 304.06 295.72 295.72 v Density 1 1 1 1 v CourantNb 0.3008 8 7.492 7.492 v FourierNb 0.16252 6.0006 0.78416 0.78416 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35865 15.464 1.7035 1.7035 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.15 304.41 295.76 295.75 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.63494 14.001 8.2762 8.2762 INSTANT 0.214000000E+02 TIME STEP NUMBER 214 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10384E-02 0.44108E-01 Friction velocity uk : 0.10384E-02 0.44108E-01 Dimensionless distance yplus : 0.35463E+00 0.15064E+02 Friction thermal sca. tstar : -0.12052E+02 0.12612E+01 Rough dim-less th. sca. tplus : 0.25178E+00 0.10695E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69996E-04 116 0.26125E+00 0.27250E-02 0.63373E+00 c Velocity[X] 0.47013E-03 c Velocity[Y] 0.22548E-02 c Velocity[Z] 0.49423E-29 c Pressure 0.32417E-03 10 0.22036E-07 0.45450E-01 0.11032E-02 c TempK 0.33998E+02 82 0.29267E-03 0.51396E-02 0.22138E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17097 0.15212 1.2841e-005 1.2841e-005 v Velocity[Y] -0.22155 0.95794 0.010918 0.010918 v Velocity[Z] -6.3956e-014 5.1454e-014 -1.1316e-016 -1.1316e-016 v ǁVelocityǁ 0.00022439 0.95946 0.06934 0.06934 v Pressure -1.0011 1.0062 -2.0428e-015 -1.4962e-015 v TempK 293.19 303.99 295.73 295.73 v Density 1 1 1 1 v CourantNb 0.2025 8 7.41 7.41 v FourierNb 0.17755 6.0359 0.79882 0.79882 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38001 17.01 1.7359 1.7359 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.19 304.06 295.77 295.76 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.44236 14.036 8.2088 8.2088 INSTANT 0.215000000E+02 TIME STEP NUMBER 215 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.54336E-03 0.45500E-01 Friction velocity uk : 0.54336E-03 0.45500E-01 Dimensionless distance yplus : 0.18557E+00 0.15540E+02 Friction thermal sca. tstar : -0.75248E+01 0.67091E+00 Rough dim-less th. sca. tplus : 0.13175E+00 0.11033E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72362E-04 116 0.29649E+00 0.29155E-02 0.66880E+00 c Velocity[X] 0.49013E-03 c Velocity[Y] 0.24253E-02 c Velocity[Z] 0.44970E-29 c Pressure 0.32685E-03 11 0.21415E-07 0.45652E-01 0.11046E-02 c TempK 0.33752E+02 81 0.35812E-03 0.49898E-02 0.20966E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20968 0.14394 2.6626e-005 2.6626e-005 v Velocity[Y] -0.21483 0.86111 0.010766 0.010766 v Velocity[Z] -6.5662e-014 5.1185e-014 -1.2032e-016 -1.2032e-016 v ǁVelocityǁ 0.00021786 0.86187 0.06847 0.06847 v Pressure -1.001 1.0056 -9.5035e-016 -4.2284e-016 v TempK 293.12 304 295.75 295.75 v Density 1 1 1 1 v CourantNb 0.16511 8 7.4253 7.4253 v FourierNb 0.1631 6.5743 0.81022 0.81022 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34815 18.711 1.7614 1.7614 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.19 303.99 295.78 295.77 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.84321 13.617 8.2355 8.2355 INSTANT 0.216000000E+02 TIME STEP NUMBER 216 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.64156E-03 0.45743E-01 Friction velocity uk : 0.64156E-03 0.45743E-01 Dimensionless distance yplus : 0.21911E+00 0.15622E+02 Friction thermal sca. tstar : -0.83118E+01 0.53999E+00 Rough dim-less th. sca. tplus : 0.15557E+00 0.11092E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70967E-04 116 0.26560E+00 0.28824E-02 0.64799E+00 c Velocity[X] 0.48977E-03 c Velocity[Y] 0.23926E-02 c Velocity[Z] 0.45243E-29 c Pressure 0.32368E-03 11 0.22126E-07 0.45782E-01 0.11217E-02 c TempK 0.33380E+02 82 0.32085E-03 0.51963E-02 0.21755E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17187 0.19127 1.5758e-005 1.5758e-005 v Velocity[Y] -0.21818 0.81059 0.010943 0.010943 v Velocity[Z] -6.655e-014 5.7378e-014 -1.0977e-016 -1.0977e-016 v ǁVelocityǁ 8.6626e-005 0.81097 0.068648 0.068648 v Pressure -1.0002 1.0073 -1.5987e-016 5.6379e-016 v TempK 292.98 303.99 295.76 295.76 v Density 1 1 1 1 v CourantNb 0.20368 8 7.4164 7.4164 v FourierNb 0.15872 7.0825 0.82042 0.82042 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33879 15.118 1.7828 1.7828 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.12 304 295.8 295.79 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0698 14.082 8.2368 8.2368 INSTANT 0.217000000E+02 TIME STEP NUMBER 217 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.41814E-03 0.44642E-01 Friction velocity uk : 0.41814E-03 0.44642E-01 Dimensionless distance yplus : 0.14281E+00 0.15247E+02 Friction thermal sca. tstar : -0.13304E+02 0.49562E+00 Rough dim-less th. sca. tplus : 0.10139E+00 0.10825E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73692E-04 116 0.28326E+00 0.32644E-02 0.70730E+00 c Velocity[X] 0.57350E-03 c Velocity[Y] 0.26909E-02 c Velocity[Z] 0.49962E-29 c Pressure 0.32589E-03 11 0.21200E-07 0.46221E-01 0.11750E-02 c TempK 0.33255E+02 83 0.45102E-03 0.50449E-02 0.21601E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16854 0.1709 2.8908e-005 2.8908e-005 v Velocity[Y] -0.24156 0.82954 0.010815 0.010815 v Velocity[Z] -7.3526e-014 4.9891e-014 -1.1784e-016 -1.1784e-016 v ǁVelocityǁ 0.00025156 0.84474 0.068464 0.068464 v Pressure -1.0015 1.007 -1.0747e-015 -4.8789e-016 v TempK 292.8 303.91 295.78 295.78 v Density 1 1 1 1 v CourantNb 0.27411 8 7.4604 7.4604 v FourierNb 0.15872 6.7995 0.83035 0.83035 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3388 14.514 1.8036 1.8036 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.98 303.99 295.81 295.8 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.5999 14.799 8.2907 8.2907 INSTANT 0.218000000E+02 TIME STEP NUMBER 218 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.45952E-03 0.42884E-01 Friction velocity uk : 0.45952E-03 0.42884E-01 Dimensionless distance yplus : 0.15694E+00 0.14646E+02 Friction thermal sca. tstar : -0.38294E+01 0.10162E+01 Rough dim-less th. sca. tplus : 0.11142E+00 0.10399E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74914E-04 115 0.27766E+00 0.31956E-02 0.71192E+00 c Velocity[X] 0.55451E-03 c Velocity[Y] 0.26411E-02 c Velocity[Z] 0.52131E-29 c Pressure 0.31623E-03 11 0.22377E-07 0.44715E-01 0.12116E-02 c TempK 0.33269E+02 82 0.36018E-03 0.54410E-02 0.21848E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15791 0.13786 1.3993e-005 1.3993e-005 v Velocity[Y] -0.25948 0.83534 0.010592 0.010592 v Velocity[Z] -6.4887e-014 5.4541e-014 -1.3931e-016 -1.3931e-016 v ǁVelocityǁ 0.00091387 0.84185 0.067598 0.067598 v Pressure -1.0025 1.0072 1.0925e-015 1.7347e-015 v TempK 292.64 304.1 295.79 295.79 v Density 1 1 1 1 v CourantNb 0.39662 8 7.5008 7.5008 v FourierNb 0.15056 7.2812 0.82992 0.82992 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36354 15.542 1.8028 1.8028 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.8 303.91 295.82 295.81 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67804 14.13 8.3308 8.3308 INSTANT 0.219000000E+02 TIME STEP NUMBER 219 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.91075E-03 0.45676E-01 Friction velocity uk : 0.91075E-03 0.45676E-01 Dimensionless distance yplus : 0.31105E+00 0.15600E+02 Friction thermal sca. tstar : -0.10854E+02 0.10080E+01 Rough dim-less th. sca. tplus : 0.22084E+00 0.11076E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74485E-04 115 0.29102E+00 0.30374E-02 0.69530E+00 c Velocity[X] 0.49106E-03 c Velocity[Y] 0.25463E-02 c Velocity[Z] 0.49285E-29 c Pressure 0.32585E-03 11 0.20975E-07 0.45963E-01 0.12534E-02 c TempK 0.33087E+02 84 0.37970E-03 0.58026E-02 0.23278E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1401 0.1548 1.4207e-005 1.4207e-005 v Velocity[Y] -0.3057 0.90589 0.010659 0.010659 v Velocity[Z] -6.1153e-014 5.1573e-014 -1.3465e-016 -1.3465e-016 v ǁVelocityǁ 0.00043213 0.91359 0.067278 0.067278 v Pressure -1.002 1.0078 -8.2601e-016 -1.7347e-016 v TempK 292.57 304 295.8 295.8 v Density 1 1 1 1 v CourantNb 0.27699 8 7.4497 7.4497 v FourierNb 0.14805 8.0094 0.83796 0.83796 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31601 17.096 1.8181 1.8181 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.64 304.1 295.84 295.83 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69388 15.953 8.2877 8.2877 INSTANT 0.220000000E+02 TIME STEP NUMBER 220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.63281E-03 0.43608E-01 Friction velocity uk : 0.63281E-03 0.43608E-01 Dimensionless distance yplus : 0.21612E+00 0.14894E+02 Friction thermal sca. tstar : -0.98564E+01 0.51968E+00 Rough dim-less th. sca. tplus : 0.15344E+00 0.10574E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74397E-04 116 0.27179E+00 0.31763E-02 0.69869E+00 c Velocity[X] 0.53490E-03 c Velocity[Y] 0.26414E-02 c Velocity[Z] 0.52253E-29 c Pressure 0.33434E-03 11 0.22056E-07 0.48309E-01 0.11579E-02 c TempK 0.32938E+02 86 0.38762E-03 0.61265E-02 0.22799E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18144 0.18776 1.4726e-005 1.4726e-005 v Velocity[Y] -0.31375 0.92889 0.010817 0.010817 v Velocity[Z] -6.4615e-014 4.7855e-014 -1.2007e-016 -1.2007e-016 v ǁVelocityǁ 0.00079915 0.92891 0.067611 0.067611 v Pressure -1.0009 1.0072 -1.6165e-015 -1.0734e-015 v TempK 292.64 303.72 295.81 295.81 v Density 1 1 1 1 v CourantNb 0.21452 8 7.4675 7.4675 v FourierNb 0.14511 7.7276 0.84227 0.84227 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31897 16.495 1.8261 1.8261 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.57 304 295.85 295.84 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57589 14.89 8.3098 8.3098 INSTANT 0.221000000E+02 TIME STEP NUMBER 221 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.19229E-03 0.45032E-01 Friction velocity uk : 0.19229E-03 0.45032E-01 Dimensionless distance yplus : 0.65673E-01 0.15380E+02 Friction thermal sca. tstar : -0.54606E+01 0.58782E+00 Rough dim-less th. sca. tplus : 0.46627E-01 0.10919E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.78076E-04 114 0.27513E+00 0.36957E-02 0.79281E+00 c Velocity[X] 0.60876E-03 c Velocity[Y] 0.30869E-02 c Velocity[Z] 0.51930E-29 c Pressure 0.32756E-03 11 0.20844E-07 0.47546E-01 0.12962E-02 c TempK 0.33130E+02 88 0.41280E-03 0.87027E-02 0.27569E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18781 0.18185 1.6634e-005 1.6634e-005 v Velocity[Y] -0.36068 0.86831 0.010536 0.010536 v Velocity[Z] -5.9187e-014 5.5558e-014 -1.499e-016 -1.499e-016 v ǁVelocityǁ 0.00047955 0.87148 0.067466 0.067466 v Pressure -1.0004 1.008 -2.3981e-016 2.7105e-016 v TempK 292.79 303.47 295.83 295.83 v Density 1 1 1 1 v CourantNb 0.41861 8 7.4894 7.4894 v FourierNb 0.15315 7.3682 0.84227 0.84227 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32692 15.728 1.8262 1.8262 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.64 303.72 295.86 295.85 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.6254 14.731 8.3317 8.3317 INSTANT 0.222000000E+02 TIME STEP NUMBER 222 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.82935E-03 0.42371E-01 Friction velocity uk : 0.82935E-03 0.42371E-01 Dimensionless distance yplus : 0.28325E+00 0.14471E+02 Friction thermal sca. tstar : -0.37052E+01 0.29089E+00 Rough dim-less th. sca. tplus : 0.20110E+00 0.10274E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79289E-04 115 0.28559E+00 0.32288E-02 0.73705E+00 c Velocity[X] 0.53000E-03 c Velocity[Y] 0.26988E-02 c Velocity[Z] 0.55963E-29 c Pressure 0.32141E-03 10 0.23612E-07 0.49201E-01 0.12681E-02 c TempK 0.33274E+02 87 0.37140E-03 0.82196E-02 0.26216E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14032 0.21326 8.1736e-007 8.1736e-007 v Velocity[Y] -0.36983 0.9405 0.01047 0.01047 v Velocity[Z] -5.7511e-014 5.4629e-014 -1.4404e-016 -1.4404e-016 v ǁVelocityǁ 0.00051986 0.94066 0.066033 0.066033 v Pressure -1.0009 1.007 -2.3981e-016 4.0115e-016 v TempK 292.94 303.3 295.84 295.84 v Density 1 1 1 1 v CourantNb 0.20813 8 7.5239 7.5239 v FourierNb 0.14981 8.105 0.82959 0.82959 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31978 17.301 1.7972 1.7972 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.79 303.47 295.88 295.87 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.52815 14.555 8.3534 8.3534 INSTANT 0.223000000E+02 TIME STEP NUMBER 223 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.27211E-03 0.42096E-01 Friction velocity uk : 0.27211E-03 0.42096E-01 Dimensionless distance yplus : 0.92934E-01 0.14377E+02 Friction thermal sca. tstar : -0.43791E+01 0.11493E+00 Rough dim-less th. sca. tplus : 0.65982E-01 0.10207E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77396E-04 114 0.26037E+00 0.28751E-02 0.66938E+00 c Velocity[X] 0.53528E-03 c Velocity[Y] 0.23398E-02 c Velocity[Z] 0.41883E-29 c Pressure 0.34725E-03 10 0.23188E-07 0.54245E-01 0.13734E-02 c TempK 0.32971E+02 88 0.34991E-03 0.90847E-02 0.27925E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16899 0.1683 1.0886e-005 1.0886e-005 v Velocity[Y] -0.27521 0.83563 0.010682 0.010682 v Velocity[Z] -5.1886e-014 5.7438e-014 -1.3363e-016 -1.3363e-016 v ǁVelocityǁ 0.00073352 0.84221 0.066649 0.066649 v Pressure -1.0012 1.0077 9.2371e-016 1.5504e-015 v TempK 293.03 303.37 295.85 295.85 v Density 1 1 1 1 v CourantNb 0.30766 8 7.3978 7.3978 v FourierNb 0.14799 6.6321 0.83372 0.83372 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3159 17.443 1.8067 1.8067 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.94 303.3 295.89 295.88 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67355 14.632 8.2316 8.2316 INSTANT 0.224000000E+02 TIME STEP NUMBER 224 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.57802E-03 0.43187E-01 Friction velocity uk : 0.57802E-03 0.43187E-01 Dimensionless distance yplus : 0.19741E+00 0.14750E+02 Friction thermal sca. tstar : -0.64274E+01 0.23795E+00 Rough dim-less th. sca. tplus : 0.14016E+00 0.10472E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 224, Physical time 0.22400E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: 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 0.79144E-04 115 0.25075E+00 0.31543E-02 0.71408E+00 c Velocity[X] 0.60764E-03 c Velocity[Y] 0.25467E-02 c Velocity[Z] 0.56973E-29 c Pressure 0.34376E-03 10 0.23075E-07 0.53328E-01 0.13317E-02 c TempK 0.32761E+02 89 0.45105E-03 0.91157E-02 0.27515E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17814 0.16173 2.764e-006 2.764e-006 v Velocity[Y] -0.25013 0.97527 0.010493 0.010493 v Velocity[Z] -5.4146e-014 5.2077e-014 -1.3714e-016 -1.3714e-016 v ǁVelocityǁ 0.00044237 0.97643 0.066092 0.066092 v Pressure -1.0021 1.0083 -1.5721e-015 -9.7578e-016 v TempK 293.05 303.65 295.85 295.85 v Density 1 1 1 1 v CourantNb 0.58947 8 7.4949 7.4949 v FourierNb 0.15971 6.8306 0.83905 0.83905 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34091 18.01 1.8181 1.8181 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.03 303.37 295.9 295.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85665 13.825 8.3339 8.3339 INSTANT 0.225000000E+02 TIME STEP NUMBER 225 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.87865E-03 0.43562E-01 Friction velocity uk : 0.87865E-03 0.43562E-01 Dimensionless distance yplus : 0.30009E+00 0.14878E+02 Friction thermal sca. tstar : -0.64891E+01 0.65269E+00 Rough dim-less th. sca. tplus : 0.21306E+00 0.10563E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81070E-04 114 0.25420E+00 0.34404E-02 0.75952E+00 c Velocity[X] 0.56202E-03 c Velocity[Y] 0.28784E-02 c Velocity[Z] 0.52525E-29 c Pressure 0.31709E-03 10 0.26378E-07 0.47184E-01 0.12765E-02 c TempK 0.32643E+02 89 0.34005E-03 0.97668E-02 0.28311E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16522 0.14222 1.6251e-005 1.6251e-005 v Velocity[Y] -0.24821 0.96463 0.010422 0.010422 v Velocity[Z] -5.2922e-014 5.9586e-014 -1.4405e-016 -1.4405e-016 v ǁVelocityǁ 0.00018574 0.96476 0.066349 0.066349 v Pressure -1.0033 1.0085 6.839e-016 1.2794e-015 v TempK 293 303.95 295.85 295.85 v Density 1 1 1 1 v CourantNb 0.21935 8 7.4652 7.4652 v FourierNb 0.16171 6.961 0.84986 0.84986 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36371 19.812 1.8409 1.8409 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.05 303.65 295.9 295.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69566 13.643 8.3151 8.3151 INSTANT 0.226000000E+02 TIME STEP NUMBER 226 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28864E-03 0.46178E-01 Friction velocity uk : 0.28864E-03 0.46178E-01 Dimensionless distance yplus : 0.98579E-01 0.15771E+02 Friction thermal sca. tstar : -0.48184E+01 0.11364E+02 Rough dim-less th. sca. tplus : 0.69989E-01 0.11197E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77228E-04 115 0.24692E+00 0.34117E-02 0.74722E+00 c Velocity[X] 0.52678E-03 c Velocity[Y] 0.28850E-02 c Velocity[Z] 0.55066E-29 c Pressure 0.31830E-03 10 0.23423E-07 0.47619E-01 0.12693E-02 c TempK 0.32679E+02 88 0.37111E-03 0.96093E-02 0.28083E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17606 0.19942 -9.4869e-007 -9.4869e-007 v Velocity[Y] -0.26416 0.93352 0.010694 0.010694 v Velocity[Z] -5.1791e-014 5.1109e-014 -1.3769e-016 -1.3769e-016 v ǁVelocityǁ 0.00021493 0.93491 0.06642 0.06642 v Pressure -1.0031 1.0078 -5.862e-016 0 v TempK 292.93 304.21 295.85 295.85 v Density 1 1 1 1 v CourantNb 0.38592 8 7.4794 7.4794 v FourierNb 0.17248 7.345 0.85377 0.85377 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36816 15.678 1.8486 1.8486 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293 303.95 295.9 295.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.56381 13.405 8.3332 8.3332 INSTANT 0.227000000E+02 TIME STEP NUMBER 227 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.24359E-03 0.41751E-01 Friction velocity uk : 0.24359E-03 0.41751E-01 Dimensionless distance yplus : 0.83194E-01 0.14259E+02 Friction thermal sca. tstar : -0.10072E+02 0.82039E+00 Rough dim-less th. sca. tplus : 0.59066E-01 0.10124E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83159E-04 113 0.25317E+00 0.34901E-02 0.76546E+00 c Velocity[X] 0.57939E-03 c Velocity[Y] 0.29107E-02 c Velocity[Z] 0.47430E-29 c Pressure 0.32519E-03 10 0.20777E-07 0.47344E-01 0.11872E-02 c TempK 0.32856E+02 88 0.47515E-03 0.10119E-01 0.28689E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.24066 0.15627 4.7021e-006 4.7021e-006 v Velocity[Y] -0.24854 0.87442 0.010496 0.010496 v Velocity[Z] -5.4746e-014 6.0022e-014 -1.477e-016 -1.477e-016 v ǁVelocityǁ 0.00049995 0.87538 0.065786 0.065786 v Pressure -1.0027 1.008 6.0396e-016 1.2577e-015 v TempK 292.87 304.56 295.86 295.86 v Density 1 1 1 1 v CourantNb 0.21114 8 7.4512 7.4512 v FourierNb 0.1667 7.1811 0.85918 0.85918 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35583 16.029 1.861 1.861 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.93 304.21 295.9 295.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75249 14.992 8.3104 8.3104 INSTANT 0.228000000E+02 TIME STEP NUMBER 228 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.67028E-03 0.46292E-01 Friction velocity uk : 0.67028E-03 0.46292E-01 Dimensionless distance yplus : 0.22892E+00 0.15810E+02 Friction thermal sca. tstar : -0.85073E+01 0.30343E+01 Rough dim-less th. sca. tplus : 0.16253E+00 0.11225E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79446E-04 114 0.24977E+00 0.32250E-02 0.73753E+00 c Velocity[X] 0.58798E-03 c Velocity[Y] 0.26370E-02 c Velocity[Z] 0.45265E-29 c Pressure 0.33142E-03 11 0.22049E-07 0.48173E-01 0.12143E-02 c TempK 0.32778E+02 87 0.33325E-03 0.10314E-01 0.28401E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19904 0.19336 -1.0986e-006 -1.0986e-006 v Velocity[Y] -0.23682 0.8622 0.01038 0.01038 v Velocity[Z] -5.0846e-014 5.4613e-014 -1.4305e-016 -1.4305e-016 v ǁVelocityǁ 0.0012336 0.86324 0.065296 0.065296 v Pressure -1.0027 1.0076 -2.7534e-016 3.0358e-016 v TempK 292.84 304.68 295.86 295.86 v Density 1 1 1 1 v CourantNb 0.31879 8 7.3818 7.3818 v FourierNb 0.16587 7.8992 0.86882 0.86882 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35405 16.861 1.8821 1.8821 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.87 304.56 295.9 295.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.70451 15.48 8.2507 8.2507 INSTANT 0.229000000E+02 TIME STEP NUMBER 229 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.91696E-03 0.39026E-01 Friction velocity uk : 0.91696E-03 0.39026E-01 Dimensionless distance yplus : 0.31317E+00 0.13329E+02 Friction thermal sca. tstar : -0.18337E+02 0.11474E+01 Rough dim-less th. sca. tplus : 0.22234E+00 0.94632E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79017E-04 113 0.23499E+00 0.31556E-02 0.72063E+00 c Velocity[X] 0.53306E-03 c Velocity[Y] 0.26226E-02 c Velocity[Z] 0.52893E-29 c Pressure 0.33076E-03 11 0.23327E-07 0.46593E-01 0.11543E-02 c TempK 0.32615E+02 88 0.49354E-03 0.97274E-02 0.26878E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.2142 0.16571 1.8714e-005 1.8714e-005 v Velocity[Y] -0.28856 0.94842 0.010398 0.010398 v Velocity[Z] -5.611e-014 6.3132e-014 -1.1659e-016 -1.1659e-016 v ǁVelocityǁ 0.00078259 0.94872 0.065006 0.065006 v Pressure -1.002 1.008 -8.7041e-016 -3.2526e-016 v TempK 292.86 304.88 295.88 295.88 v Density 1 1 1 1 v CourantNb 0.32034 8 7.3563 7.3563 v FourierNb 0.17932 8.236 0.88432 0.88432 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38277 17.58 1.9149 1.9149 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.84 304.68 295.91 295.9 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.708 16.133 8.2406 8.2406 INSTANT 0.230000000E+02 TIME STEP NUMBER 230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12065E-02 0.41434E-01 Friction velocity uk : 0.12065E-02 0.41434E-01 Dimensionless distance yplus : 0.41207E+00 0.14151E+02 Friction thermal sca. tstar : -0.12587E+02 0.22602E+01 Rough dim-less th. sca. tplus : 0.29256E+00 0.10047E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80366E-04 112 0.25543E+00 0.29419E-02 0.67719E+00 c Velocity[X] 0.50261E-03 c Velocity[Y] 0.24393E-02 c Velocity[Z] 0.52619E-29 c Pressure 0.33073E-03 11 0.19622E-07 0.45798E-01 0.11808E-02 c TempK 0.32564E+02 88 0.32823E-03 0.83738E-02 0.25042E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16263 0.16925 -8.6687e-006 -8.6687e-006 v Velocity[Y] -0.26658 1.1829 0.010691 0.010691 v Velocity[Z] -6.5923e-014 6.3924e-014 -1.2572e-016 -1.2572e-016 v ǁVelocityǁ 0.00043051 1.1859 0.064912 0.064912 v Pressure -1.0011 1.0063 7.2831e-016 1.3769e-015 v TempK 292.92 305.01 295.89 295.89 v Density 1 1 1 1 v CourantNb 0.55086 8 7.3314 7.3314 v FourierNb 0.16446 9.0513 0.89277 0.89277 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35104 19.321 1.9304 1.9304 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.86 304.88 295.92 295.91 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.90178 15.476 8.2241 8.2241 INSTANT 0.231000000E+02 TIME STEP NUMBER 231 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10946E-02 0.42959E-01 Friction velocity uk : 0.10946E-02 0.42959E-01 Dimensionless distance yplus : 0.37385E+00 0.14672E+02 Friction thermal sca. tstar : -0.76742E+01 0.12371E+01 Rough dim-less th. sca. tplus : 0.26543E+00 0.10417E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81788E-04 111 0.26457E+00 0.30223E-02 0.68253E+00 c Velocity[X] 0.54251E-03 c Velocity[Y] 0.24798E-02 c Velocity[Z] 0.50875E-29 c Pressure 0.34698E-03 10 0.20284E-07 0.46291E-01 0.10544E-02 c TempK 0.32407E+02 88 0.35752E-03 0.80359E-02 0.23877E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17793 0.17845 5.1853e-006 5.1853e-006 v Velocity[Y] -0.28558 0.90301 0.010761 0.010761 v Velocity[Z] -7.0372e-014 6.3897e-014 -1.0195e-016 -1.0195e-016 v ǁVelocityǁ 0.00077936 0.90434 0.064886 0.064886 v Pressure -1.0017 1.0055 -1.3589e-015 -6.9389e-016 v TempK 292.99 305.06 295.9 295.9 v Density 1 1 1 1 v CourantNb 0.42764 8 7.3383 7.3383 v FourierNb 0.15951 9.5047 0.90356 0.90356 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34048 20.288 1.9542 1.9542 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.92 305.01 295.93 295.92 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.77874 16.871 8.2418 8.2418 INSTANT 0.232000000E+02 TIME STEP NUMBER 232 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.82798E-03 0.42596E-01 Friction velocity uk : 0.82798E-03 0.42596E-01 Dimensionless distance yplus : 0.28278E+00 0.14548E+02 Friction thermal sca. tstar : -0.80497E+01 0.35188E+01 Rough dim-less th. sca. tplus : 0.20077E+00 0.10329E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.84777E-04 111 0.27521E+00 0.31380E-02 0.71467E+00 c Velocity[X] 0.52695E-03 c Velocity[Y] 0.26110E-02 c Velocity[Z] 0.52568E-29 c Pressure 0.33848E-03 10 0.19415E-07 0.46984E-01 0.10624E-02 c TempK 0.32347E+02 89 0.31563E-03 0.77384E-02 0.23710E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18583 0.16124 -1.172e-005 -1.172e-005 v Velocity[Y] -0.23752 0.92551 0.010619 0.010619 v Velocity[Z] -6.6595e-014 6.355e-014 -1.3316e-016 -1.3316e-016 v ǁVelocityǁ 0.00090004 0.92794 0.06422 0.06422 v Pressure -1.0033 1.0079 -1.1902e-015 -5.9631e-016 v TempK 293.08 305.31 295.91 295.91 v Density 1 1 1 1 v CourantNb 0.23247 8 7.3458 7.3458 v FourierNb 0.16469 9.5934 0.90722 0.90722 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3619 20.478 1.9624 1.9624 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 292.99 305.06 295.95 295.94 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.79232 17.593 8.253 8.253 INSTANT 0.233000000E+02 TIME STEP NUMBER 233 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.95442E-03 0.42365E-01 Friction velocity uk : 0.95442E-03 0.42365E-01 Dimensionless distance yplus : 0.32596E+00 0.14469E+02 Friction thermal sca. tstar : -0.14822E+02 0.13857E+01 Rough dim-less th. sca. tplus : 0.23143E+00 0.10273E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82355E-04 110 0.27269E+00 0.29676E-02 0.68737E+00 c Velocity[X] 0.50643E-03 c Velocity[Y] 0.24612E-02 c Velocity[Z] 0.55067E-29 c Pressure 0.33458E-03 13 0.20114E-07 0.51578E-01 0.10829E-02 c TempK 0.32204E+02 88 0.32582E-03 0.59619E-02 0.21693E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.2089 0.14843 9.736e-006 9.736e-006 v Velocity[Y] -0.22538 0.92893 0.010774 0.010774 v Velocity[Z] -6.1082e-014 6.4061e-014 -1.0422e-016 -1.0422e-016 v ǁVelocityǁ 0.00026377 0.93016 0.064019 0.064019 v Pressure -1.0033 1.0061 -1.1546e-015 -5.7463e-016 v TempK 293.18 305.21 295.92 295.92 v Density 1 1 1 1 v CourantNb 0.26045 8 7.3412 7.3412 v FourierNb 0.17355 5.3396 0.89598 0.89598 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38851 11.398 1.9387 1.9387 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.08 305.31 295.95 295.94 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.53326 13.34 8.2371 8.2371 INSTANT 0.234000000E+02 TIME STEP NUMBER 234 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.53214E-03 0.41554E-01 Friction velocity uk : 0.53214E-03 0.41554E-01 Dimensionless distance yplus : 0.18174E+00 0.14192E+02 Friction thermal sca. tstar : -0.12267E+02 0.15943E+02 Rough dim-less th. sca. tplus : 0.12903E+00 0.10076E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79051E-04 110 0.23214E+00 0.29753E-02 0.67828E+00 c Velocity[X] 0.54760E-03 c Velocity[Y] 0.24277E-02 c Velocity[Z] 0.52512E-29 c Pressure 0.33754E-03 10 0.21431E-07 0.51518E-01 0.10241E-02 c TempK 0.31928E+02 88 0.37898E-03 0.67937E-02 0.22538E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16245 0.15229 6.3489e-007 6.3489e-007 v Velocity[Y] -0.24498 0.94421 0.010759 0.010759 v Velocity[Z] -5.3207e-014 6.4172e-014 -1.2249e-016 -1.2249e-016 v ǁVelocityǁ 0.00094154 0.94438 0.063941 0.063941 v Pressure -1.0037 1.0065 -8.4377e-016 -3.5779e-016 v TempK 293.26 305.53 295.94 295.94 v Density 1 1 1 1 v CourantNb 0.41592 8 7.349 7.349 v FourierNb 0.18865 5.8213 0.9058 0.9058 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40268 12.426 1.9593 1.9593 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.18 305.21 295.97 295.96 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.94656 13.821 8.2547 8.2547 INSTANT 0.235000000E+02 TIME STEP NUMBER 235 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11555E-02 0.41993E-01 Friction velocity uk : 0.11555E-02 0.41993E-01 Dimensionless distance yplus : 0.39464E+00 0.14342E+02 Friction thermal sca. tstar : -0.57916E+01 0.15128E+01 Rough dim-less th. sca. tplus : 0.28019E+00 0.10182E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82389E-04 110 0.24957E+00 0.30263E-02 0.68553E+00 c Velocity[X] 0.55813E-03 c Velocity[Y] 0.24682E-02 c Velocity[Z] 0.52805E-29 c Pressure 0.33907E-03 10 0.22086E-07 0.52008E-01 0.11782E-02 c TempK 0.31854E+02 87 0.41043E-03 0.58981E-02 0.22404E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16436 0.1724 8.2125e-006 8.2125e-006 v Velocity[Y] -0.22861 0.91908 0.010684 0.010684 v Velocity[Z] -5.0027e-014 6.2185e-014 -1.3104e-016 -1.3104e-016 v ǁVelocityǁ 0.00068533 0.92945 0.063734 0.063734 v Pressure -1.0036 1.0076 -6.3949e-016 -5.421e-017 v TempK 293.3 305.32 295.95 295.95 v Density 1 1 1 1 v CourantNb 0.38958 8 7.3978 7.3978 v FourierNb 0.17537 6.3273 0.90895 0.90895 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39582 13.506 1.9662 1.9662 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.26 305.53 295.98 295.97 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0609 13.653 8.3067 8.3067 INSTANT 0.236000000E+02 TIME STEP NUMBER 236 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.87302E-03 0.40701E-01 Friction velocity uk : 0.87302E-03 0.40701E-01 Dimensionless distance yplus : 0.29816E+00 0.13901E+02 Friction thermal sca. tstar : -0.49476E+01 0.10252E+02 Rough dim-less th. sca. tplus : 0.21169E+00 0.98692E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81468E-04 111 0.25687E+00 0.30937E-02 0.71012E+00 c Velocity[X] 0.51906E-03 c Velocity[Y] 0.25747E-02 c Velocity[Z] 0.47634E-29 c Pressure 0.34155E-03 11 0.23874E-07 0.53205E-01 0.11141E-02 c TempK 0.31882E+02 87 0.43135E-03 0.67940E-02 0.23549E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17839 0.16367 4.2489e-006 4.2489e-006 v Velocity[Y] -0.22927 0.84034 0.010774 0.010774 v Velocity[Z] -5.6221e-014 6.3146e-014 -1.1947e-016 -1.1947e-016 v ǁVelocityǁ 0.00075523 0.84177 0.063478 0.063478 v Pressure -1.0026 1.0062 -9.0594e-016 -3.361e-016 v TempK 293.32 305.47 295.96 295.96 v Density 1 1 1 1 v CourantNb 0.24311 8 7.4005 7.4005 v FourierNb 0.17789 5.1663 0.91307 0.91307 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37972 11.028 1.9751 1.9751 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.3 305.32 295.99 295.98 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.64705 13.16 8.3136 8.3136 INSTANT 0.237000000E+02 TIME STEP NUMBER 237 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.22219E-03 0.40355E-01 Friction velocity uk : 0.22219E-03 0.40355E-01 Dimensionless distance yplus : 0.75886E-01 0.13783E+02 Friction thermal sca. tstar : -0.47216E+01 0.12771E+01 Rough dim-less th. sca. tplus : 0.53878E-01 0.97854E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80175E-04 111 0.24632E+00 0.29763E-02 0.68222E+00 c Velocity[X] 0.51321E-03 c Velocity[Y] 0.24631E-02 c Velocity[Z] 0.47697E-29 c Pressure 0.35135E-03 10 0.22081E-07 0.55537E-01 0.10845E-02 c TempK 0.31824E+02 87 0.52812E-03 0.69961E-02 0.24971E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17972 0.1727 2.6644e-005 2.6644e-005 v Velocity[Y] -0.24252 0.92915 0.010903 0.010903 v Velocity[Z] -5.5616e-014 6.2337e-014 -1.4565e-016 -1.4565e-016 v ǁVelocityǁ 0.0003346 0.92944 0.063637 0.063637 v Pressure -1.0016 1.007 -3.1974e-016 3.361e-016 v TempK 293.33 305.36 295.96 295.96 v Density 1 1 1 1 v CourantNb 0.44514 8 7.4256 7.4256 v FourierNb 0.18202 4.8377 0.91611 0.91611 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38853 10.73 1.9826 1.9826 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.32 305.47 296 295.99 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69981 12.838 8.3417 8.3417 INSTANT 0.238000000E+02 TIME STEP NUMBER 238 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.21361E-03 0.38516E-01 Friction velocity uk : 0.21361E-03 0.38516E-01 Dimensionless distance yplus : 0.72956E-01 0.13154E+02 Friction thermal sca. tstar : -0.77079E+01 0.19418E+01 Rough dim-less th. sca. tplus : 0.51797E-01 0.93394E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81723E-04 111 0.25383E+00 0.30873E-02 0.69833E+00 c Velocity[X] 0.60642E-03 c Velocity[Y] 0.24808E-02 c Velocity[Z] 0.50486E-29 c Pressure 0.35794E-03 11 0.20806E-07 0.55774E-01 0.11935E-02 c TempK 0.31939E+02 87 0.51180E-03 0.94335E-02 0.28939E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15307 0.21971 9.0689e-006 9.0689e-006 v Velocity[Y] -0.28544 0.86545 0.0108 0.0108 v Velocity[Z] -5.4468e-014 6.07e-014 -1.4457e-016 -1.4457e-016 v ǁVelocityǁ 0.00082118 0.87009 0.063078 0.063078 v Pressure -1.0006 1.0087 -3.7303e-016 1.4095e-016 v TempK 293.33 305 295.97 295.97 v Density 1 1 1 1 v CourantNb 0.2106 8 7.4489 7.4489 v FourierNb 0.15982 4.8623 0.91908 0.91908 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34114 11.803 1.9902 1.9902 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.33 305.36 296.01 296 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69505 12.676 8.368 8.368 INSTANT 0.239000000E+02 TIME STEP NUMBER 239 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.57742E-03 0.40711E-01 Friction velocity uk : 0.57742E-03 0.40711E-01 Dimensionless distance yplus : 0.19721E+00 0.13904E+02 Friction thermal sca. tstar : -0.99408E+01 0.23352E+01 Rough dim-less th. sca. tplus : 0.14001E+00 0.98717E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81278E-04 109 0.26561E+00 0.31110E-02 0.73672E+00 c Velocity[X] 0.58562E-03 c Velocity[Y] 0.25254E-02 c Velocity[Z] 0.54685E-29 c Pressure 0.34736E-03 11 0.21391E-07 0.51880E-01 0.11974E-02 c TempK 0.32079E+02 88 0.52950E-03 0.96035E-02 0.28973E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18438 0.16482 1.9151e-005 1.9151e-005 v Velocity[Y] -0.27957 0.89097 0.010623 0.010623 v Velocity[Z] -5.084e-014 5.5564e-014 -1.4037e-016 -1.4037e-016 v ǁVelocityǁ 0.00011977 0.90384 0.062237 0.062237 v Pressure -1.0001 1.0082 -1.2257e-015 -6.3968e-016 v TempK 293.34 305.13 295.97 295.97 v Density 1 1 1 1 v CourantNb 0.45352 8 7.3945 7.3945 v FourierNb 0.16438 5.3485 0.92602 0.92602 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35293 12.983 2.0064 2.0064 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.33 305 296.01 296 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.83464 12.512 8.3205 8.3205 INSTANT 0.240000000E+02 TIME STEP NUMBER 240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.69154E-03 0.45823E-01 Friction velocity uk : 0.69154E-03 0.45823E-01 Dimensionless distance yplus : 0.23618E+00 0.15650E+02 Friction thermal sca. tstar : -0.17614E+02 0.11849E+01 Rough dim-less th. sca. tplus : 0.16769E+00 0.11111E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77782E-04 110 0.23510E+00 0.27197E-02 0.65041E+00 c Velocity[X] 0.48411E-03 c Velocity[Y] 0.22356E-02 c Velocity[Z] 0.52554E-29 c Pressure 0.36081E-03 10 0.22261E-07 0.50930E-01 0.13584E-02 c TempK 0.31866E+02 88 0.42182E-03 0.98839E-02 0.29834E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1594 0.16907 8.9634e-007 8.9634e-007 v Velocity[Y] -0.31286 0.92697 0.011008 0.011008 v Velocity[Z] -6.0408e-014 5.7107e-014 -1.4661e-016 -1.4661e-016 v ǁVelocityǁ 0.00086797 0.93083 0.062221 0.062221 v Pressure -1.0016 1.0082 -7.9048e-016 -1.8431e-016 v TempK 293.35 305.01 295.97 295.97 v Density 1 1 1 1 v CourantNb 0.18185 8 7.3875 7.3875 v FourierNb 0.14951 5.8833 0.93427 0.93427 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35479 14.079 2.0252 2.0252 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.34 305.13 296.01 296 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.82771 13.655 8.3217 8.3217 INSTANT 0.241000000E+02 TIME STEP NUMBER 241 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.34362E-03 0.41737E-01 Friction velocity uk : 0.34362E-03 0.41737E-01 Dimensionless distance yplus : 0.11736E+00 0.14254E+02 Friction thermal sca. tstar : -0.82274E+01 0.18198E+01 Rough dim-less th. sca. tplus : 0.83322E-01 0.10120E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79354E-04 109 0.24183E+00 0.29831E-02 0.68356E+00 c Velocity[X] 0.59884E-03 c Velocity[Y] 0.23842E-02 c Velocity[Z] 0.54915E-29 c Pressure 0.37125E-03 11 0.20397E-07 0.49600E-01 0.12475E-02 c TempK 0.31625E+02 89 0.58431E-03 0.10744E-01 0.30003E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16797 0.18499 3.0007e-005 3.0007e-005 v Velocity[Y] -0.29865 1.0375 0.010887 0.010887 v Velocity[Z] -6.2621e-014 6.2196e-014 -1.4375e-016 -1.4375e-016 v ǁVelocityǁ 0.00055725 1.0431 0.061579 0.061579 v Pressure -1.0026 1.0088 -6.3061e-016 -7.5894e-017 v TempK 293.34 304.78 295.98 295.98 v Density 1 1 1 1 v CourantNb 0.34075 8 7.3885 7.3885 v FourierNb 0.16446 6.4717 0.95025 0.95025 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36738 15.486 2.0612 2.0612 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.35 305.01 296.01 296 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.74585 14.302 8.3387 8.3387 INSTANT 0.242000000E+02 TIME STEP NUMBER 242 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28016E-03 0.42360E-01 Friction velocity uk : 0.28016E-03 0.42360E-01 Dimensionless distance yplus : 0.95682E-01 0.14467E+02 Friction thermal sca. tstar : -0.58174E+01 0.13926E+01 Rough dim-less th. sca. tplus : 0.67932E-01 0.10272E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80976E-04 108 0.25283E+00 0.31322E-02 0.72228E+00 c Velocity[X] 0.55941E-03 c Velocity[Y] 0.25728E-02 c Velocity[Z] 0.45867E-29 c Pressure 0.35223E-03 11 0.19563E-07 0.43865E-01 0.12752E-02 c TempK 0.31446E+02 88 0.52494E-03 0.88460E-02 0.29554E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16076 0.17921 4.7592e-006 4.7592e-006 v Velocity[Y] -0.26065 0.96038 0.010763 0.010763 v Velocity[Z] -6.2799e-014 6.1031e-014 -1.3962e-016 -1.3962e-016 v ǁVelocityǁ 0.00020363 0.96066 0.061306 0.061306 v Pressure -1.003 1.0096 -1.2434e-016 4.9873e-016 v TempK 293.32 304.94 295.98 295.98 v Density 1 1 1 1 v CourantNb 0.45999 8 7.3781 7.3781 v FourierNb 0.15752 6.7715 0.97228 0.97228 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36091 17.035 2.1101 2.1101 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.34 304.78 296.02 296.01 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.86946 14.772 8.3503 8.3503 INSTANT 0.243000000E+02 TIME STEP NUMBER 243 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10444E-03 0.40569E-01 Friction velocity uk : 0.10444E-03 0.40569E-01 Dimensionless distance yplus : 0.35668E-01 0.13855E+02 Friction thermal sca. tstar : -0.38715E+02 0.13533E+01 Rough dim-less th. sca. tplus : 0.25324E-01 0.98371E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77519E-04 110 0.23831E+00 0.28522E-02 0.67399E+00 c Velocity[X] 0.47788E-03 c Velocity[Y] 0.23743E-02 c Velocity[Z] 0.50021E-29 c Pressure 0.33376E-03 11 0.19363E-07 0.39055E-01 0.12845E-02 c TempK 0.31379E+02 87 0.57088E-03 0.97004E-02 0.27589E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18078 0.13053 1.4158e-005 1.4158e-005 v Velocity[Y] -0.23294 1.034 0.01105 0.01105 v Velocity[Z] -5.1482e-014 6.1982e-014 -1.4062e-016 -1.4062e-016 v ǁVelocityǁ 0.00033945 1.0352 0.060918 0.060918 v Pressure -1.0032 1.0087 -1.6165e-015 -1.0083e-015 v TempK 293.32 304.65 296 296 v Density 1 1 1 1 v CourantNb 0.36903 8 7.3939 7.3939 v FourierNb 0.13795 7.1754 0.9875 0.9875 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29447 18.739 2.1448 2.1448 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.32 304.94 296.02 296.01 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.2057 14.636 8.3814 8.3814 INSTANT 0.244000000E+02 TIME STEP NUMBER 244 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.34288E-03 0.45838E-01 Friction velocity uk : 0.34288E-03 0.45838E-01 Dimensionless distance yplus : 0.11711E+00 0.15655E+02 Friction thermal sca. tstar : -0.15030E+02 0.15101E+01 Rough dim-less th. sca. tplus : 0.83143E-01 0.11115E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80775E-04 109 0.26360E+00 0.29237E-02 0.68295E+00 c Velocity[X] 0.47090E-03 c Velocity[Y] 0.24528E-02 c Velocity[Z] 0.47197E-29 c Pressure 0.34091E-03 10 0.18241E-07 0.39044E-01 0.11438E-02 c TempK 0.31316E+02 88 0.48332E-03 0.96688E-02 0.27215E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17031 0.17325 3.9312e-007 3.9312e-007 v Velocity[Y] -0.23352 1.1095 0.011099 0.011099 v Velocity[Z] -5.3517e-014 6.3268e-014 -1.4305e-016 -1.4305e-016 v ǁVelocityǁ 0.0008316 1.1119 0.061046 0.061046 v Pressure -1.003 1.0092 -1.8652e-016 4.5536e-016 v TempK 293.34 304.99 296 296 v Density 1 1 1 1 v CourantNb 0.30107 8 7.332 7.332 v FourierNb 0.14572 7.893 1.0036 1.0036 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32392 16.848 2.1794 2.1794 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.32 304.65 296.04 296.03 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72058 14.757 8.3356 8.3356 INSTANT 0.245000000E+02 TIME STEP NUMBER 245 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26413E-03 0.43713E-01 Friction velocity uk : 0.26413E-03 0.43713E-01 Dimensionless distance yplus : 0.90207E-01 0.14929E+02 Friction thermal sca. tstar : -0.69305E+01 0.16938E+01 Rough dim-less th. sca. tplus : 0.64045E-01 0.10600E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.83496E-04 108 0.29203E+00 0.30764E-02 0.71681E+00 c Velocity[X] 0.50498E-03 c Velocity[Y] 0.25714E-02 c Velocity[Z] 0.49338E-29 c Pressure 0.34331E-03 10 0.20475E-07 0.38125E-01 0.13153E-02 c TempK 0.31343E+02 88 0.37838E-03 0.96237E-02 0.26941E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19514 0.14183 1.982e-005 1.982e-005 v Velocity[Y] -0.21936 0.94237 0.010943 0.010943 v Velocity[Z] -5.2114e-014 6.2179e-014 -1.4376e-016 -1.4376e-016 v ǁVelocityǁ 0.00037336 0.94267 0.060354 0.060354 v Pressure -1.0026 1.0098 -8.9706e-016 -4.2284e-016 v TempK 293.36 305.04 296.01 296.01 v Density 1 1 1 1 v CourantNb 0.39639 8 7.3733 7.3733 v FourierNb 0.16029 8.6823 1.0016 1.0016 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35631 18.533 2.1742 2.1742 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.34 304.99 296.04 296.04 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60855 15.774 8.3749 8.3749 INSTANT 0.246000000E+02 TIME STEP NUMBER 246 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.76822E-03 0.42982E-01 Friction velocity uk : 0.76822E-03 0.42982E-01 Dimensionless distance yplus : 0.26237E+00 0.14680E+02 Friction thermal sca. tstar : -0.20081E+02 0.11858E+01 Rough dim-less th. sca. tplus : 0.18628E+00 0.10422E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79977E-04 108 0.25807E+00 0.25765E-02 0.63413E+00 c Velocity[X] 0.46537E-03 c Velocity[Y] 0.21111E-02 c Velocity[Z] 0.49030E-29 c Pressure 0.33656E-03 10 0.16701E-07 0.35098E-01 0.12916E-02 c TempK 0.31135E+02 87 0.42158E-03 0.76501E-02 0.24163E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21573 0.1477 1.3645e-005 1.3645e-005 v Velocity[Y] -0.19799 1.0029 0.011012 0.011012 v Velocity[Z] -5.3448e-014 6.0729e-014 -1.4312e-016 -1.4312e-016 v ǁVelocityǁ 0.00032404 1.0061 0.05998 0.05998 v Pressure -1.0026 1.0083 -3.7303e-016 2.06e-016 v TempK 293.36 304.85 296.02 296.02 v Density 1 1 1 1 v CourantNb 0.36106 8 7.2994 7.2994 v FourierNb 0.17632 9.5505 1.0138 1.0138 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39194 20.386 2.2017 2.2017 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.36 305.04 296.05 296.05 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.79243 17.362 8.3132 8.3132 INSTANT 0.247000000E+02 TIME STEP NUMBER 247 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10632E-02 0.42806E-01 Friction velocity uk : 0.10632E-02 0.42806E-01 Dimensionless distance yplus : 0.36312E+00 0.14619E+02 Friction thermal sca. tstar : -0.47934E+01 0.96839E+00 Rough dim-less th. sca. tplus : 0.25781E+00 0.10380E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.82367E-04 109 0.26538E+00 0.29105E-02 0.68124E+00 c Velocity[X] 0.47443E-03 c Velocity[Y] 0.24361E-02 c Velocity[Z] 0.46179E-29 c Pressure 0.35642E-03 11 0.19120E-07 0.37354E-01 0.11197E-02 c TempK 0.31000E+02 89 0.50350E-03 0.11073E-01 0.27489E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19093 0.16799 1.2163e-005 1.2163e-005 v Velocity[Y] -0.23564 0.92101 0.010844 0.010844 v Velocity[Z] -4.897e-014 6.2912e-014 -1.025e-016 -1.025e-016 v ǁVelocityǁ 0.00029675 0.92764 0.059966 0.059966 v Pressure -1.0019 1.0063 -7.0166e-016 -8.6736e-017 v TempK 293.31 304.61 296.03 296.03 v Density 1 1 1 1 v CourantNb 0.035771 8 7.2601 7.2601 v FourierNb 0.18958 10 1.0198 1.0198 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40713 21.346 2.2146 2.2146 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.36 304.85 296.06 296.05 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.24053 17.75 8.2799 8.2799 INSTANT 0.248000000E+02 TIME STEP NUMBER 248 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10103E-02 0.46159E-01 Friction velocity uk : 0.10103E-02 0.46159E-01 Dimensionless distance yplus : 0.34505E+00 0.15765E+02 Friction thermal sca. tstar : -0.77787E+01 0.20804E+01 Rough dim-less th. sca. tplus : 0.24498E+00 0.11193E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80865E-04 111 0.28665E+00 0.28076E-02 0.68781E+00 c Velocity[X] 0.47123E-03 c Velocity[Y] 0.23363E-02 c Velocity[Z] 0.49621E-29 c Pressure 0.34160E-03 10 0.14851E-07 0.34085E-01 0.10835E-02 c TempK 0.30977E+02 88 0.32581E-03 0.13350E-01 0.30896E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18776 0.16177 -4.1248e-006 -4.1248e-006 v Velocity[Y] -0.22138 0.84576 0.010784 0.010784 v Velocity[Z] -5.197e-014 6.0062e-014 -1.1964e-016 -1.1964e-016 v ǁVelocityǁ 0.00028789 0.84753 0.059127 0.059127 v Pressure -1.0007 1.0059 -4.6185e-016 1.8431e-016 v TempK 293.24 304.64 296.03 296.03 v Density 1 1 1 1 v CourantNb 0.29355 8 7.2718 7.2718 v FourierNb 0.17884 10 1.0334 1.0334 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40241 21.346 2.2457 2.2457 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.31 304.61 296.07 296.06 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81075 17.584 8.3052 8.3052 INSTANT 0.249000000E+02 TIME STEP NUMBER 249 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.60145E-03 0.40398E-01 Friction velocity uk : 0.60145E-03 0.40398E-01 Dimensionless distance yplus : 0.20541E+00 0.13797E+02 Friction thermal sca. tstar : -0.25565E+02 0.42348E+01 Rough dim-less th. sca. tplus : 0.14584E+00 0.97958E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77148E-04 109 0.24171E+00 0.26874E-02 0.64622E+00 c Velocity[X] 0.48413E-03 c Velocity[Y] 0.22032E-02 c Velocity[Z] 0.53519E-29 c Pressure 0.33909E-03 11 0.17743E-07 0.36295E-01 0.10192E-02 c TempK 0.30796E+02 90 0.46496E-03 0.11540E-01 0.29425E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20377 0.14996 4.3663e-006 4.3663e-006 v Velocity[Y] -0.26705 0.97155 0.010826 0.010826 v Velocity[Z] -4.9868e-014 6.039e-014 -1.0134e-016 -1.0134e-016 v ǁVelocityǁ 0.00026534 0.97559 0.059406 0.059406 v Pressure -1 1.0058 -1.0925e-015 -4.8789e-016 v TempK 293.18 304.42 296.04 296.04 v Density 1 1 1 1 v CourantNb 0.30056 8 7.2727 7.2727 v FourierNb 0.1921 10 1.0353 1.0353 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41005 21.346 2.2456 2.2456 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.24 304.64 296.07 296.06 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.50793 17.163 8.3081 8.3081 INSTANT 0.250000000E+02 TIME STEP NUMBER 250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.84672E-03 0.44120E-01 Friction velocity uk : 0.84672E-03 0.44120E-01 Dimensionless distance yplus : 0.28918E+00 0.15068E+02 Friction thermal sca. tstar : -0.66907E+01 0.30441E+01 Rough dim-less th. sca. tplus : 0.20531E+00 0.10698E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79856E-04 111 0.26376E+00 0.27598E-02 0.67751E+00 c Velocity[X] 0.47631E-03 c Velocity[Y] 0.22835E-02 c Velocity[Z] 0.52579E-29 c Pressure 0.33201E-03 10 0.17463E-07 0.35820E-01 0.10345E-02 c TempK 0.30741E+02 90 0.39814E-03 0.10896E-01 0.28487E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.2086 0.15804 2.387e-007 2.387e-007 v Velocity[Y] -0.26145 0.96521 0.010613 0.010613 v Velocity[Z] -5.193e-014 6.0326e-014 -1.2412e-016 -1.2412e-016 v ǁVelocityǁ 0.00026674 0.96523 0.058648 0.058648 v Pressure -1.0001 1.006 -3.908e-016 2.1684e-016 v TempK 293.19 304.4 296.06 296.06 v Density 1 1 1 1 v CourantNb 0.2134 8 7.3178 7.3178 v FourierNb 0.16692 10 1.0364 1.0364 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40814 21.346 2.2483 2.2483 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.18 304.42 296.08 296.07 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.665 17.341 8.3542 8.3542 INSTANT 0.251000000E+02 TIME STEP NUMBER 251 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.45387E-03 0.46113E-01 Friction velocity uk : 0.45387E-03 0.46113E-01 Dimensionless distance yplus : 0.15501E+00 0.15749E+02 Friction thermal sca. tstar : -0.13340E+02 0.11641E+01 Rough dim-less th. sca. tplus : 0.11005E+00 0.11182E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77780E-04 112 0.24390E+00 0.25125E-02 0.62592E+00 c Velocity[X] 0.44301E-03 c Velocity[Y] 0.20695E-02 c Velocity[Z] 0.55673E-29 c Pressure 0.34100E-03 11 0.20009E-07 0.37642E-01 0.11407E-02 c TempK 0.30542E+02 89 0.46218E-03 0.13830E-01 0.32384E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21174 0.14808 8.5746e-007 8.5746e-007 v Velocity[Y] -0.22487 1.0952 0.010845 0.010845 v Velocity[Z] -5.7263e-014 5.6667e-014 -1.3593e-016 -1.3593e-016 v ǁVelocityǁ 0.00042792 1.0954 0.05838 0.05838 v Pressure -1.0002 1.0052 -2.6645e-017 5.421e-016 v TempK 293.23 304.33 296.09 296.09 v Density 1 1 1 1 v CourantNb 0.097313 8 7.2547 7.2547 v FourierNb 0.18361 10 1.0271 1.0271 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40642 21.346 2.2283 2.2283 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.19 304.4 296.1 296.1 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0129 17.775 8.2818 8.2818 INSTANT 0.252000000E+02 TIME STEP NUMBER 252 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.47567E-03 0.44557E-01 Friction velocity uk : 0.47567E-03 0.44557E-01 Dimensionless distance yplus : 0.16246E+00 0.15218E+02 Friction thermal sca. tstar : -0.40571E+01 0.96881E+00 Rough dim-less th. sca. tplus : 0.11534E+00 0.10804E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.78001E-04 110 0.25258E+00 0.27149E-02 0.65507E+00 c Velocity[X] 0.48692E-03 c Velocity[Y] 0.22279E-02 c Velocity[Z] 0.50735E-29 c Pressure 0.34642E-03 10 0.18942E-07 0.39024E-01 0.10430E-02 c TempK 0.30345E+02 88 0.47323E-03 0.15177E-01 0.36282E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21323 0.19131 -2.4795e-005 -2.4795e-005 v Velocity[Y] -0.19264 0.94856 0.010785 0.010785 v Velocity[Z] -6.0046e-014 5.3427e-014 -1.5323e-016 -1.5323e-016 v ǁVelocityǁ 0.00036118 0.94898 0.058224 0.058224 v Pressure -1.0002 1.0068 -1.3323e-016 5.0958e-016 v TempK 293.26 304 296.12 296.12 v Density 1 1 1 1 v CourantNb 0.20453 8 7.2588 7.2588 v FourierNb 0.16271 10 1.0336 1.0336 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40868 21.346 2.2396 2.2396 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.23 304.33 296.13 296.13 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.9491 17.61 8.2923 8.2923 INSTANT 0.253000000E+02 TIME STEP NUMBER 253 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.71706E-03 0.44081E-01 Friction velocity uk : 0.71706E-03 0.44081E-01 Dimensionless distance yplus : 0.24490E+00 0.15055E+02 Friction thermal sca. tstar : -0.90654E+01 0.16264E+01 Rough dim-less th. sca. tplus : 0.17387E+00 0.10689E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76913E-04 112 0.24569E+00 0.27623E-02 0.67882E+00 c Velocity[X] 0.45516E-03 c Velocity[Y] 0.23071E-02 c Velocity[Z] 0.55748E-29 c Pressure 0.34078E-03 10 0.18782E-07 0.39166E-01 0.10452E-02 c TempK 0.30390E+02 86 0.44575E-03 0.12289E-01 0.30597E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17834 0.18671 -1.0285e-005 -1.0285e-005 v Velocity[Y] -0.17867 0.91363 0.010891 0.010891 v Velocity[Z] -5.7081e-014 5.2516e-014 -1.3632e-016 -1.3632e-016 v ǁVelocityǁ 0.00043749 0.91838 0.057899 0.057899 v Pressure -1.0002 1.0059 -5.1514e-016 1.9516e-016 v TempK 293.25 303.78 296.15 296.15 v Density 1 1 1 1 v CourantNb 0.20158 8 7.2608 7.2608 v FourierNb 0.11698 10 1.0441 1.0441 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33292 21.346 2.2633 2.2633 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.26 304 296.16 296.15 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.76425 17.454 8.3049 8.3049 INSTANT 0.254000000E+02 TIME STEP NUMBER 254 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.34686E-03 0.43287E-01 Friction velocity uk : 0.34686E-03 0.43287E-01 Dimensionless distance yplus : 0.11846E+00 0.14784E+02 Friction thermal sca. tstar : -0.17162E+02 0.10145E+01 Rough dim-less th. sca. tplus : 0.84107E-01 0.10496E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77114E-04 112 0.26134E+00 0.26894E-02 0.64881E+00 c Velocity[X] 0.49172E-03 c Velocity[Y] 0.21976E-02 c Velocity[Z] 0.51085E-29 c Pressure 0.36119E-03 10 0.18092E-07 0.41237E-01 0.10455E-02 c TempK 0.30424E+02 92 0.59917E-03 0.11844E-01 0.29200E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1856 0.20574 -1.1525e-005 -1.1525e-005 v Velocity[Y] -0.19114 0.86001 0.010915 0.010915 v Velocity[Z] -5.2822e-014 5.4152e-014 -1.5035e-016 -1.5035e-016 v ǁVelocityǁ 0.00024273 0.8607 0.058516 0.058516 v Pressure -1.0001 1.0066 -9.77e-016 -4.4452e-016 v TempK 293.18 303.7 296.17 296.17 v Density 1 1 1 1 v CourantNb 0.15502 8 7.2274 7.2274 v FourierNb 0.12867 10 1.0494 1.0494 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36621 21.346 2.2765 2.2765 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.25 303.78 296.18 296.18 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.30764 16.338 8.2768 8.2768 INSTANT 0.255000000E+02 TIME STEP NUMBER 255 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.51543E-03 0.42862E-01 Friction velocity uk : 0.51543E-03 0.42862E-01 Dimensionless distance yplus : 0.17603E+00 0.14638E+02 Friction thermal sca. tstar : -0.63662E+01 0.35719E+01 Rough dim-less th. sca. tplus : 0.12498E+00 0.10393E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79104E-04 112 0.25659E+00 0.28253E-02 0.69019E+00 c Velocity[X] 0.49248E-03 c Velocity[Y] 0.23328E-02 c Velocity[Z] 0.59625E-29 c Pressure 0.34196E-03 11 0.18206E-07 0.39104E-01 0.12587E-02 c TempK 0.30611E+02 86 0.43417E-03 0.10351E-01 0.28089E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.22303 0.15438 -1.7896e-006 -1.7896e-006 v Velocity[Y] -0.18316 1.0678 0.01081 0.01081 v Velocity[Z] -5.02e-014 5.7129e-014 -1.3787e-016 -1.3787e-016 v ǁVelocityǁ 0.00069369 1.0679 0.057573 0.057573 v Pressure -1 1.0075 -5.5955e-016 1.0842e-017 v TempK 293.11 303.53 296.2 296.2 v Density 1 1 1 1 v CourantNb 0.46947 8 7.3039 7.3039 v FourierNb 0.14154 10 1.0415 1.0415 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40284 21.346 2.262 2.262 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.18 303.7 296.21 296.2 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.131 16.99 8.3454 8.3454 INSTANT 0.256000000E+02 TIME STEP NUMBER 256 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.50554E-03 0.43110E-01 Friction velocity uk : 0.50554E-03 0.43110E-01 Dimensionless distance yplus : 0.17266E+00 0.14723E+02 Friction thermal sca. tstar : -0.84750E+01 0.78803E+00 Rough dim-less th. sca. tplus : 0.12258E+00 0.10453E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75983E-04 112 0.26325E+00 0.27395E-02 0.67779E+00 c Velocity[X] 0.45401E-03 c Velocity[Y] 0.22855E-02 c Velocity[Z] 0.57667E-29 c Pressure 0.35666E-03 11 0.18592E-07 0.39498E-01 0.13170E-02 c TempK 0.30388E+02 87 0.41741E-03 0.10250E-01 0.27065E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20999 0.18876 -5.1306e-006 -5.1306e-006 v Velocity[Y] -0.20066 1.004 0.010734 0.010734 v Velocity[Z] -5.6088e-014 5.2169e-014 -1.3834e-016 -1.3834e-016 v ǁVelocityǁ 0.00057772 1.0044 0.057487 0.057487 v Pressure -0.99981 1.0052 1.3589e-015 2.0383e-015 v TempK 293.1 303.51 296.23 296.23 v Density 1 1 1 1 v CourantNb 0.058565 8 7.2259 7.2259 v FourierNb 0.15569 10 1.045 1.045 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.43112 21.346 2.2696 2.2696 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.11 303.53 296.24 296.23 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.33684 17.342 8.2709 8.2709 INSTANT 0.257000000E+02 TIME STEP NUMBER 257 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.67769E-03 0.43512E-01 Friction velocity uk : 0.67769E-03 0.43512E-01 Dimensionless distance yplus : 0.23145E+00 0.14861E+02 Friction thermal sca. tstar : -0.27111E+02 0.48323E+00 Rough dim-less th. sca. tplus : 0.16433E+00 0.10551E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76078E-04 113 0.25045E+00 0.25978E-02 0.65435E+00 c Velocity[X] 0.47078E-03 c Velocity[Y] 0.21270E-02 c Velocity[Z] 0.56534E-29 c Pressure 0.35156E-03 10 0.18318E-07 0.39923E-01 0.11007E-02 c TempK 0.30110E+02 87 0.36905E-03 0.93815E-02 0.25333E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20717 0.17895 7.5546e-006 7.5546e-006 v Velocity[Y] -0.19796 0.86664 0.010745 0.010745 v Velocity[Z] -5.8237e-014 5.4556e-014 -1.5491e-016 -1.5491e-016 v ǁVelocityǁ 0.00028715 0.86922 0.057515 0.057515 v Pressure -0.99963 1.0053 -4.7073e-016 1.301e-016 v TempK 293.15 303.26 296.25 296.25 v Density 1 1 1 1 v CourantNb 0.19136 8 7.2706 7.2706 v FourierNb 0.17126 10 1.0383 1.0383 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41244 21.346 2.2555 2.2555 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.1 303.51 296.26 296.26 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.42824 16.943 8.3089 8.3089 INSTANT 0.258000000E+02 TIME STEP NUMBER 258 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.89008E-04 0.44259E-01 Friction velocity uk : 0.89008E-04 0.44259E-01 Dimensionless distance yplus : 0.30399E-01 0.15116E+02 Friction thermal sca. tstar : -0.49196E+01 0.10126E+00 Rough dim-less th. sca. tplus : 0.21583E-01 0.10732E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75583E-04 113 0.26862E+00 0.26690E-02 0.65901E+00 c Velocity[X] 0.48607E-03 c Velocity[Y] 0.21829E-02 c Velocity[Z] 0.57328E-29 c Pressure 0.34460E-03 10 0.18901E-07 0.38949E-01 0.11079E-02 c TempK 0.29877E+02 87 0.35292E-03 0.89072E-02 0.25798E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19502 0.14197 4.5114e-007 4.5114e-007 v Velocity[Y] -0.21065 0.92724 0.010766 0.010766 v Velocity[Z] -5.8771e-014 5.9102e-014 -1.1545e-016 -1.1545e-016 v ǁVelocityǁ 0.00082939 0.92835 0.057429 0.057429 v Pressure -0.9994 1.0053 -7.6383e-016 -1.6263e-016 v TempK 293.21 303.18 296.26 296.26 v Density 1 1 1 1 v CourantNb 0.41195 8 7.2627 7.2627 v FourierNb 0.1873 10 1.0398 1.0398 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39979 21.346 2.2564 2.2564 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.15 303.26 296.28 296.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.76661 16.655 8.3025 8.3025 INSTANT 0.259000000E+02 TIME STEP NUMBER 259 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.48682E-03 0.43641E-01 Friction velocity uk : 0.48682E-03 0.43641E-01 Dimensionless distance yplus : 0.16626E+00 0.14905E+02 Friction thermal sca. tstar : -0.50989E+01 0.26818E-01 Rough dim-less th. sca. tplus : 0.11805E+00 0.10582E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74333E-04 112 0.27317E+00 0.26595E-02 0.65346E+00 c Velocity[X] 0.48729E-03 c Velocity[Y] 0.21722E-02 c Velocity[Z] 0.55820E-29 c Pressure 0.35021E-03 11 0.17522E-07 0.39955E-01 0.10338E-02 c TempK 0.29655E+02 88 0.38684E-03 0.84002E-02 0.24229E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16256 0.14815 3.4932e-006 3.4932e-006 v Velocity[Y] -0.25235 0.92999 0.010823 0.010823 v Velocity[Z] -5.8393e-014 5.4681e-014 -1.4782e-016 -1.4782e-016 v ǁVelocityǁ 4.2352e-005 0.93132 0.057886 0.057886 v Pressure -0.99952 1.006 4.7962e-016 1.03e-015 v TempK 293.25 302.95 296.27 296.27 v Density 1 1 1 1 v CourantNb 0.33366 8 7.3142 7.3142 v FourierNb 0.18329 10 1.0421 1.0421 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40447 21.346 2.2595 2.2595 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.21 303.18 296.3 296.29 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.80045 17.008 8.3563 8.3563 INSTANT 0.260000000E+02 TIME STEP NUMBER 260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.50338E-03 0.46349E-01 Friction velocity uk : 0.50338E-03 0.46349E-01 Dimensionless distance yplus : 0.17192E+00 0.15829E+02 Friction thermal sca. tstar : -0.18266E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.12206E+00 0.11239E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74280E-04 113 0.26946E+00 0.27543E-02 0.66947E+00 c Velocity[X] 0.47573E-03 c Velocity[Y] 0.22785E-02 c Velocity[Z] 0.54585E-29 c Pressure 0.34510E-03 16 0.17175E-07 0.39229E-01 0.10588E-02 c TempK 0.29562E+02 89 0.33316E-03 0.78624E-02 0.24083E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16301 0.15408 -1.1691e-005 -1.1691e-005 v Velocity[Y] -0.27576 1.044 0.010861 0.010861 v Velocity[Z] -5.7305e-014 5.7133e-014 -1.2371e-016 -1.2371e-016 v ǁVelocityǁ 0.00037073 1.0446 0.057898 0.057898 v Pressure -0.99975 1.0057 -6.3061e-016 -1.0842e-016 v TempK 293.25 302.94 296.27 296.27 v Density 1 1 1 1 v CourantNb 0.22702 8 7.372 7.372 v FourierNb 0.18555 10 1.05 1.05 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.4167 21.346 2.2771 2.2771 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.25 303.15 296.31 296.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.96915 17.948 8.4219 8.4219 INSTANT 0.261000000E+02 TIME STEP NUMBER 261 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.37901E-03 0.43184E-01 Friction velocity uk : 0.37901E-03 0.43184E-01 Dimensionless distance yplus : 0.12944E+00 0.14748E+02 Friction thermal sca. tstar : -0.99764E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.91902E-01 0.10471E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75408E-04 112 0.29158E+00 0.27206E-02 0.65898E+00 c Velocity[X] 0.43602E-03 c Velocity[Y] 0.22846E-02 c Velocity[Z] 0.52922E-29 c Pressure 0.35426E-03 10 0.19871E-07 0.39981E-01 0.12219E-02 c TempK 0.29578E+02 90 0.34567E-03 0.79004E-02 0.22554E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20572 0.1806 -7.8203e-007 -7.8203e-007 v Velocity[Y] -0.2757 0.96218 0.01113 0.01113 v Velocity[Z] -5.6017e-014 5.7882e-014 -1.362e-016 -1.362e-016 v ǁVelocityǁ 0.00044798 0.96275 0.057615 0.057615 v Pressure -1.0018 1.0067 -8.793e-016 -3.361e-016 v TempK 293.23 303.04 296.27 296.27 v Density 1 1 1 1 v CourantNb 0.098291 8 7.3431 7.3431 v FourierNb 0.15688 10 1.0592 1.0592 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34088 21.346 2.2963 2.2963 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.25 303.15 296.31 296.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.3727 17.952 8.4023 8.4023 INSTANT 0.262000000E+02 TIME STEP NUMBER 262 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.75270E-03 0.51086E-01 Friction velocity uk : 0.75270E-03 0.51086E-01 Dimensionless distance yplus : 0.25707E+00 0.17448E+02 Friction thermal sca. tstar : -0.38328E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.18252E+00 0.12387E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75302E-04 112 0.28523E+00 0.26479E-02 0.65125E+00 c Velocity[X] 0.45805E-03 c Velocity[Y] 0.21898E-02 c Velocity[Z] 0.43237E-29 c Pressure 0.36138E-03 11 0.16918E-07 0.40281E-01 0.11604E-02 c TempK 0.29368E+02 90 0.36931E-03 0.77123E-02 0.23528E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18513 0.17637 -9.9167e-006 -9.9167e-006 v Velocity[Y] -0.28124 1.0107 0.011073 0.011073 v Velocity[Z] -5.8777e-014 5.882e-014 -1.1771e-016 -1.1771e-016 v ǁVelocityǁ 0.00044295 1.0109 0.057601 0.057601 v Pressure -1.0031 1.006 -9.9476e-016 -2.4937e-016 v TempK 293.26 303.26 296.27 296.27 v Density 1 1 1 1 v CourantNb 0.41155 8 7.3457 7.3457 v FourierNb 0.12155 10 1.0712 1.0712 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34594 21.346 2.3206 2.3206 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.23 303.15 296.31 296.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.79456 17.531 8.4169 8.4169 INSTANT 0.263000000E+02 TIME STEP NUMBER 263 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.29446E-03 0.43244E-01 Friction velocity uk : 0.29446E-03 0.43244E-01 Dimensionless distance yplus : 0.10057E+00 0.14769E+02 Friction thermal sca. tstar : -0.65609E+01 0.98835E-01 Rough dim-less th. sca. tplus : 0.71402E-01 0.10486E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75243E-04 112 0.27509E+00 0.27377E-02 0.67502E+00 c Velocity[X] 0.49010E-03 c Velocity[Y] 0.22476E-02 c Velocity[Z] 0.46578E-29 c Pressure 0.34974E-03 10 0.17419E-07 0.37777E-01 0.11571E-02 c TempK 0.29217E+02 90 0.38953E-03 0.81596E-02 0.24459E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16475 0.18001 -9.2736e-006 -9.2736e-006 v Velocity[Y] -0.25903 0.94955 0.010735 0.010735 v Velocity[Z] -6.2475e-014 6.2202e-014 -1.3129e-016 -1.3129e-016 v ǁVelocityǁ 0.00061592 0.95138 0.05714 0.05714 v Pressure -1.0026 1.0047 -1.1724e-015 -5.5294e-016 v TempK 293.33 303.45 296.29 296.29 v Density 1 1 1 1 v CourantNb 0.54875 8 7.3725 7.3725 v FourierNb 0.1337 10 1.0884 1.0884 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37127 21.346 2.3579 2.3579 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.26 303.26 296.31 296.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.98483 16.576 8.4608 8.4608 INSTANT 0.264000000E+02 TIME STEP NUMBER 264 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11354E-03 0.45746E-01 Friction velocity uk : 0.11354E-03 0.45746E-01 Dimensionless distance yplus : 0.38779E-01 0.15624E+02 Friction thermal sca. tstar : -0.98488E+01 0.58641E+00 Rough dim-less th. sca. tplus : 0.27532E-01 0.11092E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76922E-04 112 0.29359E+00 0.25909E-02 0.65547E+00 c Velocity[X] 0.43863E-03 c Velocity[Y] 0.21523E-02 c Velocity[Z] 0.52982E-29 c Pressure 0.32735E-03 10 0.14682E-07 0.33775E-01 0.11015E-02 c TempK 0.29233E+02 89 0.29219E-03 0.83728E-02 0.24355E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.172 0.13839 -2.6334e-005 -2.6334e-005 v Velocity[Y] -0.21905 0.91127 0.010857 0.010857 v Velocity[Z] -6.3942e-014 6.2671e-014 -1.345e-016 -1.345e-016 v ǁVelocityǁ 0.00049543 0.91413 0.056994 0.056994 v Pressure -1.0022 1.0056 5.1514e-016 1.095e-015 v TempK 293.44 303.7 296.3 296.3 v Density 1 1 1 1 v CourantNb 0.50973 8 7.393 7.393 v FourierNb 0.14707 10 1.1106 1.1106 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38242 21.346 2.4048 2.4048 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.33 303.45 296.33 296.32 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1418 17.386 8.5036 8.5036 INSTANT 0.265000000E+02 TIME STEP NUMBER 265 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10615E-02 0.42956E-01 Friction velocity uk : 0.10615E-02 0.42956E-01 Dimensionless distance yplus : 0.36254E+00 0.14671E+02 Friction thermal sca. tstar : -0.46179E+01 0.11141E+01 Rough dim-less th. sca. tplus : 0.25739E+00 0.10416E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73886E-04 115 0.26535E+00 0.27882E-02 0.66497E+00 c Velocity[X] 0.45095E-03 c Velocity[Y] 0.23373E-02 c Velocity[Z] 0.49262E-29 c Pressure 0.34366E-03 10 0.14485E-07 0.35358E-01 0.10142E-02 c TempK 0.29122E+02 89 0.36136E-03 0.69211E-02 0.22690E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16796 0.12691 -9.1256e-006 -9.1256e-006 v Velocity[Y] -0.27539 1.1118 0.010951 0.010951 v Velocity[Z] -6.348e-014 6.2512e-014 -1.4727e-016 -1.4727e-016 v ǁVelocityǁ 0.00047068 1.112 0.057282 0.057282 v Pressure -1.0021 1.0057 -9.4147e-016 -4.2284e-016 v TempK 293.51 303.82 296.32 296.32 v Density 1 1 1 1 v CourantNb 0.25609 8 7.4593 7.4593 v FourierNb 0.16178 10 1.1169 1.1169 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40375 21.346 2.4182 2.4182 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.44 303.7 296.34 296.33 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0392 17.842 8.5762 8.5762 INSTANT 0.266000000E+02 TIME STEP NUMBER 266 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.95444E-03 0.41676E-01 Friction velocity uk : 0.95444E-03 0.41676E-01 Dimensionless distance yplus : 0.32597E+00 0.14234E+02 Friction thermal sca. tstar : -0.15155E+02 0.11601E+01 Rough dim-less th. sca. tplus : 0.23143E+00 0.10106E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79631E-04 111 0.29734E+00 0.30798E-02 0.74710E+00 c Velocity[X] 0.44965E-03 c Velocity[Y] 0.26302E-02 c Velocity[Z] 0.47445E-29 c Pressure 0.32111E-03 10 0.13703E-07 0.32916E-01 0.10265E-02 c TempK 0.29249E+02 90 0.30107E-03 0.70639E-02 0.23647E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15018 0.15745 -1.427e-005 -1.427e-005 v Velocity[Y] -0.18424 1.0239 0.010737 0.010737 v Velocity[Z] -6.5148e-014 6.0749e-014 -1.0841e-016 -1.0841e-016 v ǁVelocityǁ 0.00044819 1.0241 0.056818 0.056818 v Pressure -1.0021 1.008 -1.5987e-015 -1.0192e-015 v TempK 293.53 304.07 296.33 296.33 v Density 1 1 1 1 v CourantNb 0.46994 8 7.486 7.486 v FourierNb 0.16268 10 1.1256 1.1256 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41134 21.346 2.4364 2.4364 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.51 303.82 296.36 296.35 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89764 16.58 8.6116 8.6116 INSTANT 0.267000000E+02 TIME STEP NUMBER 267 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13890E-02 0.41920E-01 Friction velocity uk : 0.13890E-02 0.41920E-01 Dimensionless distance yplus : 0.47437E+00 0.14317E+02 Friction thermal sca. tstar : -0.62007E+01 0.19730E+01 Rough dim-less th. sca. tplus : 0.33680E+00 0.10165E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76060E-04 113 0.27678E+00 0.26640E-02 0.68424E+00 c Velocity[X] 0.42008E-03 c Velocity[Y] 0.22440E-02 c Velocity[Z] 0.47509E-29 c Pressure 0.32330E-03 10 0.13515E-07 0.34010E-01 0.96376E-03 c TempK 0.29115E+02 88 0.35310E-03 0.67643E-02 0.24730E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17485 0.15269 2.2483e-007 2.2483e-007 v Velocity[Y] -0.19957 0.87667 0.010795 0.010795 v Velocity[Z] -6.3634e-014 5.9367e-014 -1.5417e-016 -1.5417e-016 v ǁVelocityǁ 0.00059083 0.87669 0.056767 0.056767 v Pressure -1.0019 1.0047 -1.4122e-015 -9.1073e-016 v TempK 293.52 304.04 296.34 296.34 v Density 1 1 1 1 v CourantNb 0.26565 8 7.5399 7.5399 v FourierNb 0.16742 10 1.1159 1.1159 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40279 21.346 2.4164 2.4164 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.53 304.07 296.37 296.36 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.83249 16.737 8.6559 8.6559 INSTANT 0.268000000E+02 TIME STEP NUMBER 268 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.49372E-03 0.40685E-01 Friction velocity uk : 0.49372E-03 0.40685E-01 Dimensionless distance yplus : 0.16862E+00 0.13895E+02 Friction thermal sca. tstar : -0.97572E+01 0.22096E+01 Rough dim-less th. sca. tplus : 0.11972E+00 0.98654E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74308E-04 111 0.26428E+00 0.26040E-02 0.66879E+00 c Velocity[X] 0.44435E-03 c Velocity[Y] 0.21597E-02 c Velocity[Z] 0.42020E-29 c Pressure 0.31924E-03 10 0.11701E-07 0.33120E-01 0.85581E-03 c TempK 0.28956E+02 89 0.31336E-03 0.68801E-02 0.24195E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17838 0.13675 -7.2165e-006 -7.2165e-006 v Velocity[Y] -0.23787 0.93359 0.010666 0.010666 v Velocity[Z] -6.2673e-014 6.1891e-014 -1.1614e-016 -1.1614e-016 v ǁVelocityǁ 0.00080371 0.93722 0.05667 0.05667 v Pressure -1.0018 1.0056 -3.5527e-016 2.4937e-016 v TempK 293.49 304.13 296.35 296.35 v Density 1 1 1 1 v CourantNb 0.39691 8 7.5696 7.5696 v FourierNb 0.18416 10 1.1251 1.1251 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3986 22.478 2.4367 2.4367 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.52 304.04 296.38 296.37 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81171 17.873 8.6948 8.6948 INSTANT 0.269000000E+02 TIME STEP NUMBER 269 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.80255E-03 0.40036E-01 Friction velocity uk : 0.80255E-03 0.40036E-01 Dimensionless distance yplus : 0.27410E+00 0.13673E+02 Friction thermal sca. tstar : -0.88992E+01 0.86691E+00 Rough dim-less th. sca. tplus : 0.19460E+00 0.97079E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72634E-04 110 0.25724E+00 0.26827E-02 0.68193E+00 c Velocity[X] 0.43797E-03 c Velocity[Y] 0.22447E-02 c Velocity[Z] 0.45607E-29 c Pressure 0.31782E-03 10 0.14441E-07 0.32933E-01 0.94518E-03 c TempK 0.28932E+02 90 0.42405E-03 0.78511E-02 0.26430E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17254 0.13461 1.8808e-005 1.8808e-005 v Velocity[Y] -0.309 0.80996 0.010702 0.010702 v Velocity[Z] -6.0951e-014 6.5189e-014 -1.3533e-016 -1.3533e-016 v ǁVelocityǁ 0.00047511 0.81051 0.056759 0.056759 v Pressure -1.001 1.0059 -8.1712e-016 -3.0358e-016 v TempK 293.47 304.1 296.36 296.36 v Density 1 1 1 1 v CourantNb 0.32349 8 7.6088 7.6088 v FourierNb 0.19529 10 1.1259 1.1259 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41686 21.346 2.4362 2.4362 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.49 304.13 296.39 296.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69668 17.199 8.7347 8.7347 INSTANT 0.270000000E+02 TIME STEP NUMBER 270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.35100E-03 0.41070E-01 Friction velocity uk : 0.35100E-03 0.41070E-01 Dimensionless distance yplus : 0.11988E+00 0.14027E+02 Friction thermal sca. tstar : -0.15540E+02 0.91848E+00 Rough dim-less th. sca. tplus : 0.85110E-01 0.99587E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74346E-04 111 0.26794E+00 0.25822E-02 0.66456E+00 c Velocity[X] 0.42281E-03 c Velocity[Y] 0.21594E-02 c Velocity[Z] 0.42746E-29 c Pressure 0.31187E-03 11 0.12933E-07 0.30898E-01 0.99772E-03 c TempK 0.28884E+02 90 0.37907E-03 0.83284E-02 0.26516E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17189 0.1456 -9.4519e-006 -9.4519e-006 v Velocity[Y] -0.3169 0.84437 0.010853 0.010853 v Velocity[Z] -5.8539e-014 6.0081e-014 -1.3248e-016 -1.3248e-016 v ǁVelocityǁ 0.00069057 0.84504 0.056739 0.056739 v Pressure -1.0002 1.0053 -7.2831e-016 -8.6736e-017 v TempK 293.46 304.01 296.37 296.37 v Density 1 1 1 1 v CourantNb 0.10441 8 7.6048 7.6048 v FourierNb 0.19188 10 1.1305 1.1305 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.42249 22.656 2.4467 2.4467 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.47 304.1 296.4 296.39 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.63481 16.954 8.7353 8.7353 INSTANT 0.271000000E+02 TIME STEP NUMBER 271 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.74301E-03 0.40888E-01 Friction velocity uk : 0.74301E-03 0.40888E-01 Dimensionless distance yplus : 0.25376E+00 0.13965E+02 Friction thermal sca. tstar : -0.65555E+01 0.17387E+01 Rough dim-less th. sca. tplus : 0.18016E+00 0.99146E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74030E-04 111 0.26192E+00 0.26421E-02 0.67190E+00 c Velocity[X] 0.42241E-03 c Velocity[Y] 0.22197E-02 c Velocity[Z] 0.43121E-29 c Pressure 0.33268E-03 10 0.11434E-07 0.32096E-01 0.85887E-03 c TempK 0.28844E+02 91 0.46034E-03 0.10700E-01 0.29491E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17377 0.13418 1.4523e-005 1.4523e-005 v Velocity[Y] -0.26006 0.84576 0.010928 0.010928 v Velocity[Z] -6.1756e-014 5.9992e-014 -1.1682e-016 -1.1682e-016 v ǁVelocityǁ 0.0010109 0.85582 0.056504 0.056504 v Pressure -1.0009 1.0062 3.1086e-016 8.9989e-016 v TempK 293.46 304.13 296.38 296.38 v Density 1 1 1 1 v CourantNb 0.48342 8 7.6193 7.6193 v FourierNb 0.15936 10 1.1221 1.1221 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38143 24.922 2.4282 2.4282 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.46 304.01 296.41 296.4 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0858 17.228 8.7414 8.7414 INSTANT 0.272000000E+02 TIME STEP NUMBER 272 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.80393E-03 0.46218E-01 Friction velocity uk : 0.80393E-03 0.46218E-01 Dimensionless distance yplus : 0.27456E+00 0.15785E+02 Friction thermal sca. tstar : -0.47020E+01 0.82459E+00 Rough dim-less th. sca. tplus : 0.19494E+00 0.11207E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74433E-04 110 0.26971E+00 0.26051E-02 0.66447E+00 c Velocity[X] 0.42449E-03 c Velocity[Y] 0.21806E-02 c Velocity[Z] 0.45639E-29 c Pressure 0.32163E-03 9 0.13824E-07 0.32061E-01 0.89021E-03 c TempK 0.28699E+02 92 0.39501E-03 0.11457E-01 0.30340E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14589 0.16293 -1.575e-005 -1.575e-005 v Velocity[Y] -0.29405 0.81661 0.010827 0.010827 v Velocity[Z] -6.2964e-014 6.11e-014 -1.337e-016 -1.337e-016 v ǁVelocityǁ 0.00022398 0.822 0.056307 0.056307 v Pressure -1.002 1.0058 9.0594e-016 1.4528e-015 v TempK 293.46 304.25 296.38 296.38 v Density 1 1 1 1 v CourantNb 0.41334 8 7.6188 7.6188 v FourierNb 0.17529 10 1.1318 1.1318 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41957 21.346 2.4495 2.4495 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.46 304.13 296.42 296.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85259 17.838 8.7507 8.7507 INSTANT 0.273000000E+02 TIME STEP NUMBER 273 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.20723E-03 0.39521E-01 Friction velocity uk : 0.20723E-03 0.39521E-01 Dimensionless distance yplus : 0.70776E-01 0.13498E+02 Friction thermal sca. tstar : -0.86016E+01 0.12445E+01 Rough dim-less th. sca. tplus : 0.50250E-01 0.95831E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72787E-04 110 0.26425E+00 0.25650E-02 0.64647E+00 c Velocity[X] 0.40815E-03 c Velocity[Y] 0.21568E-02 c Velocity[Z] 0.48741E-29 c Pressure 0.32034E-03 10 0.13577E-07 0.32599E-01 0.95029E-03 c TempK 0.28604E+02 92 0.39261E-03 0.10762E-01 0.27966E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14316 0.13878 1.3003e-005 1.3003e-005 v Velocity[Y] -0.28937 0.94292 0.010909 0.010909 v Velocity[Z] -6.252e-014 6.3208e-014 -1.1917e-016 -1.1917e-016 v ǁVelocityǁ 0.0001964 0.94425 0.056131 0.056131 v Pressure -1.0022 1.0054 -1.7852e-015 -1.2577e-015 v TempK 293.45 304.25 296.38 296.38 v Density 1 1 1 1 v CourantNb 0.68046 8 7.6134 7.6134 v FourierNb 0.19153 10 1.1329 1.1329 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40884 21.346 2.4504 2.4504 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.46 304.25 296.42 296.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.97988 17.01 8.7463 8.7463 INSTANT 0.274000000E+02 TIME STEP NUMBER 274 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.47315E-03 0.43389E-01 Friction velocity uk : 0.47315E-03 0.43389E-01 Dimensionless distance yplus : 0.16159E+00 0.14819E+02 Friction thermal sca. tstar : -0.60872E+01 0.85680E+00 Rough dim-less th. sca. tplus : 0.11473E+00 0.10521E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74980E-04 111 0.26520E+00 0.27278E-02 0.67904E+00 c Velocity[X] 0.43064E-03 c Velocity[Y] 0.22971E-02 c Velocity[Z] 0.45058E-29 c Pressure 0.33468E-03 10 0.13339E-07 0.34810E-01 0.95660E-03 c TempK 0.28583E+02 92 0.47137E-03 0.10623E-01 0.28311E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15984 0.16452 -1.0844e-005 -1.0844e-005 v Velocity[Y] -0.25322 0.90236 0.010893 0.010893 v Velocity[Z] -5.636e-014 5.9976e-014 -1.1092e-016 -1.1092e-016 v ǁVelocityǁ 0.00066195 0.90942 0.056571 0.056571 v Pressure -1.002 1.0057 -3.7303e-016 2.1684e-016 v TempK 293.45 304.35 296.38 296.38 v Density 1 1 1 1 v CourantNb 0.37758 8 7.5657 7.5657 v FourierNb 0.17845 10 1.1413 1.1413 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38091 21.346 2.4693 2.4693 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.45 304.25 296.42 296.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.93893 15.914 8.707 8.707 INSTANT 0.275000000E+02 TIME STEP NUMBER 275 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10664E-02 0.43247E-01 Friction velocity uk : 0.10664E-02 0.43247E-01 Dimensionless distance yplus : 0.36422E+00 0.14770E+02 Friction thermal sca. tstar : -0.54338E+01 0.15896E+01 Rough dim-less th. sca. tplus : 0.25859E+00 0.10487E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75952E-04 114 0.28721E+00 0.28792E-02 0.71974E+00 c Velocity[X] 0.45230E-03 c Velocity[Y] 0.24269E-02 c Velocity[Z] 0.44982E-29 c Pressure 0.32050E-03 10 0.11999E-07 0.33033E-01 0.89483E-03 c TempK 0.28868E+02 94 0.40609E-03 0.12991E-01 0.30845E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16036 0.22323 1.1538e-005 1.1538e-005 v Velocity[Y] -0.21911 0.90172 0.01079 0.01079 v Velocity[Z] -6.2351e-014 5.881e-014 -1.2899e-016 -1.2899e-016 v ǁVelocityǁ 0.00054087 0.92894 0.056163 0.056163 v Pressure -1.0019 1.0049 -8.5265e-016 -2.6021e-016 v TempK 293.47 304.45 296.37 296.37 v Density 1 1 1 1 v CourantNb 0.734 8 7.6322 7.6322 v FourierNb 0.1543 10 1.1486 1.1486 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36892 21.346 2.4867 2.4867 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.45 304.35 296.42 296.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1729 16.451 8.7808 8.7808 INSTANT 0.276000000E+02 TIME STEP NUMBER 276 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.36708E-03 0.44677E-01 Friction velocity uk : 0.36708E-03 0.44677E-01 Dimensionless distance yplus : 0.12537E+00 0.15259E+02 Friction thermal sca. tstar : -0.79432E+01 0.99050E+00 Rough dim-less th. sca. tplus : 0.89009E-01 0.10833E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76245E-04 110 0.26921E+00 0.27406E-02 0.70142E+00 c Velocity[X] 0.46747E-03 c Velocity[Y] 0.22731E-02 c Velocity[Z] 0.49594E-29 c Pressure 0.33197E-03 9 0.13843E-07 0.34037E-01 0.10605E-02 c TempK 0.28983E+02 94 0.50422E-03 0.13904E-01 0.33341E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17544 0.18516 -3.9113e-005 -3.9113e-005 v Velocity[Y] -0.21389 0.95373 0.010864 0.010864 v Velocity[Z] -5.8933e-014 5.6915e-014 -1.4446e-016 -1.4446e-016 v ǁVelocityǁ 0.00092557 0.97154 0.055688 0.055688 v Pressure -1.0015 1.0075 -2.6645e-016 2.8189e-016 v TempK 293.53 304.34 296.36 296.36 v Density 1 1 1 1 v CourantNb 0.49111 8 7.5895 7.5895 v FourierNb 0.14399 10 1.1471 1.1471 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39047 23.463 2.4838 2.4838 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.47 304.45 296.41 296.4 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.74986 17.332 8.7367 8.7367 INSTANT 0.277000000E+02 TIME STEP NUMBER 277 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.15935E-03 0.38664E-01 Friction velocity uk : 0.15935E-03 0.38664E-01 Dimensionless distance yplus : 0.54422E-01 0.13205E+02 Friction thermal sca. tstar : -0.46210E+01 0.85747E+00 Rough dim-less th. sca. tplus : 0.38639E-01 0.93753E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73663E-04 108 0.25374E+00 0.27041E-02 0.68752E+00 c Velocity[X] 0.49294E-03 c Velocity[Y] 0.22112E-02 c Velocity[Z] 0.52969E-29 c Pressure 0.34143E-03 9 0.17392E-07 0.34061E-01 0.11995E-02 c TempK 0.28856E+02 94 0.43390E-03 0.12839E-01 0.30163E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17471 0.1795 -1.9873e-005 -1.9873e-005 v Velocity[Y] -0.2561 0.82953 0.010853 0.010853 v Velocity[Z] -6.1505e-014 5.6073e-014 -1.2641e-016 -1.2641e-016 v ǁVelocityǁ 0.00032212 0.83076 0.055362 0.055362 v Pressure -1.0007 1.0076 -1.4744e-015 -8.8905e-016 v TempK 293.61 304.3 296.35 296.35 v Density 1 1 1 1 v CourantNb 0.17766 8 7.5081 7.5081 v FourierNb 0.15839 10 1.1659 1.1659 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41885 21.346 2.5244 2.5244 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.53 304.34 296.4 296.39 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.53655 17.876 8.6741 8.6741 INSTANT 0.278000000E+02 TIME STEP NUMBER 278 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.66834E-03 0.44411E-01 Friction velocity uk : 0.66834E-03 0.44411E-01 Dimensionless distance yplus : 0.22826E+00 0.15168E+02 Friction thermal sca. tstar : -0.76994E+01 0.53160E+01 Rough dim-less th. sca. tplus : 0.16206E+00 0.10769E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75463E-04 113 0.27139E+00 0.25669E-02 0.66455E+00 c Velocity[X] 0.47406E-03 c Velocity[Y] 0.20928E-02 c Velocity[Z] 0.50303E-29 c Pressure 0.33067E-03 10 0.13447E-07 0.32333E-01 0.10566E-02 c TempK 0.28788E+02 94 0.33786E-03 0.10931E-01 0.28101E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16366 0.18987 -2.3924e-005 -2.3924e-005 v Velocity[Y] -0.2774 0.83274 0.010966 0.010966 v Velocity[Z] -6.2254e-014 5.6688e-014 -9.8133e-017 -9.8133e-017 v ǁVelocityǁ 0.00046109 0.83343 0.055213 0.055213 v Pressure -1.0002 1.0056 -3.6415e-016 2.1684e-016 v TempK 293.67 304.48 296.35 296.35 v Density 1 1 1 1 v CourantNb 0.42461 8 7.4779 7.4779 v FourierNb 0.16406 10 1.1829 1.1829 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3845 21.346 2.5604 2.5604 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.61 304.3 296.39 296.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.70116 16.759 8.6608 8.6608 INSTANT 0.279000000E+02 TIME STEP NUMBER 279 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.51019E-03 0.44274E-01 Friction velocity uk : 0.51019E-03 0.44274E-01 Dimensionless distance yplus : 0.17424E+00 0.15121E+02 Friction thermal sca. tstar : -0.11450E+02 0.15153E+01 Rough dim-less th. sca. tplus : 0.12371E+00 0.10736E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73517E-04 109 0.25823E+00 0.25257E-02 0.64805E+00 c Velocity[X] 0.46116E-03 c Velocity[Y] 0.20646E-02 c Velocity[Z] 0.57277E-29 c Pressure 0.33927E-03 10 0.13965E-07 0.31315E-01 0.10805E-02 c TempK 0.28826E+02 94 0.49512E-03 0.10367E-01 0.27286E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1805 0.20963 -1.6883e-005 -1.6883e-005 v Velocity[Y] -0.25025 0.89725 0.011159 0.011159 v Velocity[Z] -6.9697e-014 5.8609e-014 -1.0678e-016 -1.0678e-016 v ǁVelocityǁ 0.00035658 0.91151 0.055255 0.055255 v Pressure -1.0007 1.0055 -8.2601e-016 -1.1926e-016 v TempK 293.69 304.5 296.35 296.35 v Density 1 1 1 1 v CourantNb 0.21045 8 7.4424 7.4424 v FourierNb 0.15678 10 1.2057 1.2057 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33465 21.552 2.611 2.611 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.67 304.48 296.38 296.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.64961 17.707 8.6481 8.6481 INSTANT 0.280000000E+02 TIME STEP NUMBER 280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.47623E-03 0.42976E-01 Friction velocity uk : 0.47623E-03 0.42976E-01 Dimensionless distance yplus : 0.16265E+00 0.14678E+02 Friction thermal sca. tstar : -0.48868E+01 0.11106E+01 Rough dim-less th. sca. tplus : 0.11548E+00 0.10421E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76682E-04 109 0.27164E+00 0.26836E-02 0.66021E+00 c Velocity[X] 0.49156E-03 c Velocity[Y] 0.21920E-02 c Velocity[Z] 0.50875E-29 c Pressure 0.34931E-03 9 0.14408E-07 0.32030E-01 0.11507E-02 c TempK 0.28793E+02 93 0.38540E-03 0.93655E-02 0.26930E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18859 0.17758 -3.598e-005 -3.598e-005 v Velocity[Y] -0.34684 0.91908 0.010991 0.010991 v Velocity[Z] -6.8522e-014 6.4442e-014 -1.1104e-016 -1.1104e-016 v ǁVelocityǁ 0.00057253 0.91923 0.054891 0.054891 v Pressure -1.0009 1.0073 -1.4744e-015 -8.3484e-016 v TempK 293.7 304.39 296.36 296.36 v Density 1 1 1 1 v CourantNb 0.30979 8 7.46 7.46 v FourierNb 0.17245 10 1.2264 1.2264 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36811 21.346 2.6569 2.6569 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.69 304.5 296.39 296.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.97272 17.022 8.6864 8.6864 INSTANT 0.281000000E+02 TIME STEP NUMBER 281 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.30307E-03 0.44237E-01 Friction velocity uk : 0.30307E-03 0.44237E-01 Dimensionless distance yplus : 0.10351E+00 0.15108E+02 Friction thermal sca. tstar : -0.64889E+01 0.93561E+00 Rough dim-less th. sca. tplus : 0.73490E-01 0.10727E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75331E-04 109 0.26736E+00 0.27570E-02 0.67213E+00 c Velocity[X] 0.47872E-03 c Velocity[Y] 0.22783E-02 c Velocity[Z] 0.53930E-29 c Pressure 0.35390E-03 10 0.12385E-07 0.31543E-01 0.11179E-02 c TempK 0.28759E+02 92 0.49942E-03 0.90038E-02 0.25059E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1662 0.15777 -1.024e-005 -1.024e-005 v Velocity[Y] -0.35045 0.91664 0.01094 0.01094 v Velocity[Z] -7.0909e-014 6.8262e-014 -1.3098e-016 -1.3098e-016 v ǁVelocityǁ 0.0002889 0.91819 0.055054 0.055054 v Pressure -1.0004 1.0055 -1.9273e-015 -1.2685e-015 v TempK 293.71 304.26 296.38 296.38 v Density 1 1 1 1 v CourantNb 0.26672 8 7.3854 7.3854 v FourierNb 0.17724 10 1.2454 1.2454 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40493 21.485 2.6979 2.6979 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.7 304.39 296.4 296.39 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81562 16.843 8.6308 8.6308 INSTANT 0.282000000E+02 TIME STEP NUMBER 282 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.50942E-03 0.43196E-01 Friction velocity uk : 0.50942E-03 0.43196E-01 Dimensionless distance yplus : 0.17398E+00 0.14753E+02 Friction thermal sca. tstar : -0.14905E+02 0.84087E+00 Rough dim-less th. sca. tplus : 0.12352E+00 0.10474E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76903E-04 109 0.25894E+00 0.26787E-02 0.68016E+00 c Velocity[X] 0.48161E-03 c Velocity[Y] 0.21971E-02 c Velocity[Z] 0.47700E-29 c Pressure 0.34784E-03 10 0.13406E-07 0.30208E-01 0.10445E-02 c TempK 0.28873E+02 91 0.42841E-03 0.85821E-02 0.26420E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19822 0.18112 -3.3918e-005 -3.3918e-005 v Velocity[Y] -0.26509 0.87597 0.010837 0.010837 v Velocity[Z] -6.5697e-014 5.6807e-014 -1.3763e-016 -1.3763e-016 v ǁVelocityǁ 0.00021051 0.88866 0.054718 0.054718 v Pressure -1.0011 1.008 -8.1712e-016 -1.9516e-016 v TempK 293.74 304.21 296.39 296.39 v Density 1 1 1 1 v CourantNb 0.26901 8 7.4057 7.4057 v FourierNb 0.16389 10 1.262 1.262 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36863 23.633 2.7357 2.7357 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.71 304.26 296.42 296.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72002 16.651 8.6678 8.6678 INSTANT 0.283000000E+02 TIME STEP NUMBER 283 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28214E-03 0.44823E-01 Friction velocity uk : 0.28214E-03 0.44823E-01 Dimensionless distance yplus : 0.96359E-01 0.15308E+02 Friction thermal sca. tstar : -0.19844E+02 0.82493E+00 Rough dim-less th. sca. tplus : 0.68413E-01 0.10869E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75993E-04 109 0.25797E+00 0.26422E-02 0.67069E+00 c Velocity[X] 0.51817E-03 c Velocity[Y] 0.21240E-02 c Velocity[Z] 0.53075E-29 c Pressure 0.35610E-03 10 0.12179E-07 0.29593E-01 0.10320E-02 c TempK 0.28748E+02 89 0.44707E-03 0.84054E-02 0.26330E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19094 0.15692 -1.5401e-005 -1.5401e-005 v Velocity[Y] -0.30799 0.83722 0.010753 0.010753 v Velocity[Z] -6.3759e-014 5.9923e-014 -1.1759e-016 -1.1759e-016 v ǁVelocityǁ 0.00025733 0.83821 0.054576 0.054576 v Pressure -1.0022 1.0062 -9.3259e-016 -2.6021e-016 v TempK 293.78 304.21 296.42 296.42 v Density 1 1 1 1 v CourantNb 0.21041 8 7.4509 7.4509 v FourierNb 0.18028 10 1.2722 1.2722 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40549 25.996 2.7562 2.7562 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.74 304.21 296.43 296.43 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67056 17.65 8.723 8.723 INSTANT 0.284000000E+02 TIME STEP NUMBER 284 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.40885E-03 0.47107E-01 Friction velocity uk : 0.40885E-03 0.47107E-01 Dimensionless distance yplus : 0.13964E+00 0.16088E+02 Friction thermal sca. tstar : -0.93589E+01 0.83678E+00 Rough dim-less th. sca. tplus : 0.99139E-01 0.11422E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75162E-04 111 0.25055E+00 0.26837E-02 0.67603E+00 c Velocity[X] 0.53019E-03 c Velocity[Y] 0.21535E-02 c Velocity[Z] 0.49886E-29 c Pressure 0.32875E-03 15 0.13082E-07 0.26692E-01 0.98993E-03 c TempK 0.28716E+02 90 0.55316E-03 0.91505E-02 0.27151E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17708 0.19197 -2.3595e-005 -2.3595e-005 v Velocity[Y] -0.34462 0.85771 0.010686 0.010686 v Velocity[Z] -6.4694e-014 6.4373e-014 -1.3142e-016 -1.3142e-016 v ǁVelocityǁ 0.00017514 0.85771 0.054585 0.054585 v Pressure -1.0026 1.0075 -2.4869e-016 3.1442e-016 v TempK 293.79 304.18 296.45 296.45 v Density 1 1 1 1 v CourantNb 0.3046 8 7.5013 7.5013 v FourierNb 0.18454 10 1.2832 1.2832 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.4187 28.461 2.7816 2.7816 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.78 304.21 296.46 296.45 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69874 17.536 8.7845 8.7845 INSTANT 0.285000000E+02 TIME STEP NUMBER 285 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.55580E-03 0.43911E-01 Friction velocity uk : 0.55580E-03 0.43911E-01 Dimensionless distance yplus : 0.18982E+00 0.14997E+02 Friction thermal sca. tstar : -0.27159E+02 0.86488E+00 Rough dim-less th. sca. tplus : 0.13477E+00 0.10648E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74890E-04 110 0.26470E+00 0.28741E-02 0.72661E+00 c Velocity[X] 0.47648E-03 c Velocity[Y] 0.23976E-02 c Velocity[Z] 0.54218E-29 c Pressure 0.31919E-03 10 0.99893E-08 0.25747E-01 0.10684E-02 c TempK 0.28824E+02 89 0.50183E-03 0.94925E-02 0.26408E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16066 0.14771 1.142e-005 1.142e-005 v Velocity[Y] -0.32925 0.87467 0.01088 0.01088 v Velocity[Z] -6.0293e-014 6.0439e-014 -1.0316e-016 -1.0316e-016 v ǁVelocityǁ 9.1672e-005 0.87886 0.054577 0.054577 v Pressure -1.0022 1.009 -4.885e-016 1.8431e-016 v TempK 293.77 304.09 296.48 296.48 v Density 1 1 1 1 v CourantNb 0.34254 8 7.481 7.481 v FourierNb 0.13563 10 1.2938 1.2938 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35008 22.185 2.801 2.801 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.79 304.18 296.49 296.48 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.54553 17.6 8.7748 8.7748 INSTANT 0.286000000E+02 TIME STEP NUMBER 286 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26453E-03 0.46364E-01 Friction velocity uk : 0.26453E-03 0.46364E-01 Dimensionless distance yplus : 0.90346E-01 0.15835E+02 Friction thermal sca. tstar : -0.97239E+01 0.80077E+00 Rough dim-less th. sca. tplus : 0.64144E-01 0.11242E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74597E-04 112 0.25334E+00 0.26741E-02 0.67634E+00 c Velocity[X] 0.42917E-03 c Velocity[Y] 0.22450E-02 c Velocity[Z] 0.51124E-29 c Pressure 0.31991E-03 10 0.10916E-07 0.26034E-01 0.11831E-02 c TempK 0.28816E+02 90 0.40483E-03 0.84699E-02 0.25215E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15682 0.12206 -1.4643e-005 -1.4643e-005 v Velocity[Y] -0.29499 0.9352 0.010937 0.010937 v Velocity[Z] -5.8039e-014 5.9175e-014 -1.406e-016 -1.406e-016 v ǁVelocityǁ 0.00046164 0.93633 0.054084 0.054084 v Pressure -1.0019 1.0057 -1.6875e-016 3.9031e-016 v TempK 293.74 303.94 296.51 296.51 v Density 1 1 1 1 v CourantNb 0.21449 8 7.4132 7.4132 v FourierNb 0.13341 10 1.2992 1.2992 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38509 21.346 2.8106 2.8106 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.77 304.09 296.52 296.51 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.48231 17.849 8.7124 8.7124 INSTANT 0.287000000E+02 TIME STEP NUMBER 287 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.47397E-03 0.45284E-01 Friction velocity uk : 0.47397E-03 0.45284E-01 Dimensionless distance yplus : 0.16187E+00 0.15466E+02 Friction thermal sca. tstar : -0.57020E+01 0.69532E+00 Rough dim-less th. sca. tplus : 0.11493E+00 0.10981E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74133E-04 114 0.26156E+00 0.25428E-02 0.65142E+00 c Velocity[X] 0.41157E-03 c Velocity[Y] 0.21312E-02 c Velocity[Z] 0.47198E-29 c Pressure 0.32974E-03 11 0.10889E-07 0.26157E-01 0.96656E-03 c TempK 0.28628E+02 92 0.45653E-03 0.92568E-02 0.24662E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15913 0.13378 -9.5227e-006 -9.5227e-006 v Velocity[Y] -0.31019 1.1615 0.011087 0.011087 v Velocity[Z] -5.8848e-014 5.888e-014 -1.3721e-016 -1.3721e-016 v ǁVelocityǁ 0.00039736 1.1628 0.054145 0.054145 v Pressure -1.0018 1.0054 -1.0658e-015 -4.9873e-016 v TempK 293.73 303.73 296.54 296.54 v Density 1 1 1 1 v CourantNb 0.088686 8 7.3673 7.3673 v FourierNb 0.14675 10 1.3188 1.3188 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39524 21.66 2.8549 2.8549 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.74 303.94 296.55 296.54 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.51674 17.963 8.6861 8.6861 INSTANT 0.288000000E+02 TIME STEP NUMBER 288 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.52875E-03 0.46017E-01 Friction velocity uk : 0.52875E-03 0.46017E-01 Dimensionless distance yplus : 0.18058E+00 0.15716E+02 Friction thermal sca. tstar : -0.18914E+02 0.57205E+00 Rough dim-less th. sca. tplus : 0.12821E+00 0.11158E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79897E-04 112 0.28520E+00 0.28076E-02 0.68706E+00 c Velocity[X] 0.46511E-03 c Velocity[Y] 0.23425E-02 c Velocity[Z] 0.48501E-29 c Pressure 0.33503E-03 10 0.13291E-07 0.26983E-01 0.10594E-02 c TempK 0.28403E+02 91 0.48994E-03 0.10314E-01 0.27867E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15842 0.15442 -2.7351e-005 -2.7351e-005 v Velocity[Y] -0.31426 1.0477 0.011021 0.011021 v Velocity[Z] -6.268e-014 6.2669e-014 -1.4681e-016 -1.4681e-016 v ǁVelocityǁ 0.00012969 1.0477 0.05465 0.05465 v Pressure -1.0017 1.0063 2.5757e-016 8.782e-016 v TempK 293.76 303.38 296.56 296.56 v Density 1 1 1 1 v CourantNb 0.059656 8 7.4249 7.4249 v FourierNb 0.16142 10 1.3196 1.3196 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41028 23.826 2.8586 2.8586 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.73 303.73 296.58 296.57 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.23844 17.962 8.7445 8.7445 INSTANT 0.289000000E+02 TIME STEP NUMBER 289 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28873E-03 0.45413E-01 Friction velocity uk : 0.28873E-03 0.45413E-01 Dimensionless distance yplus : 0.98610E-01 0.15510E+02 Friction thermal sca. tstar : -0.52857E+01 0.38082E+00 Rough dim-less th. sca. tplus : 0.70012E-01 0.11012E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77077E-04 112 0.27153E+00 0.27883E-02 0.69705E+00 c Velocity[X] 0.45121E-03 c Velocity[Y] 0.23371E-02 c Velocity[Z] 0.50502E-29 c Pressure 0.32018E-03 11 0.12899E-07 0.26391E-01 0.96787E-03 c TempK 0.28464E+02 90 0.43276E-03 0.66895E-02 0.22858E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1716 0.15019 6.8151e-006 6.8151e-006 v Velocity[Y] -0.27822 1.0082 0.010982 0.010982 v Velocity[Z] -6.4516e-014 6.6775e-014 -1.1372e-016 -1.1372e-016 v ǁVelocityǁ 2.3426e-005 1.0087 0.054068 0.054068 v Pressure -1.0016 1.006 -2.6645e-017 6.7221e-016 v TempK 293.83 303.28 296.58 296.58 v Density 1 1 1 1 v CourantNb 0.24868 8 7.4606 7.4606 v FourierNb 0.1541 10 1.319 1.319 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40434 26.023 2.8587 2.8587 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.76 303.38 296.6 296.59 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.70744 17.683 8.7796 8.7796 INSTANT 0.290000000E+02 TIME STEP NUMBER 290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.69505E-03 0.54331E-01 Friction velocity uk : 0.69505E-03 0.54331E-01 Dimensionless distance yplus : 0.23738E+00 0.18556E+02 Friction thermal sca. tstar : -0.75219E+01 0.21337E+00 Rough dim-less th. sca. tplus : 0.16854E+00 0.13174E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77551E-04 112 0.26659E+00 0.27076E-02 0.66830E+00 c Velocity[X] 0.43649E-03 c Velocity[Y] 0.22711E-02 c Velocity[Z] 0.51135E-29 c Pressure 0.33468E-03 11 0.11328E-07 0.28080E-01 0.89925E-03 c TempK 0.28336E+02 90 0.45477E-03 0.83963E-02 0.25055E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.216 0.17419 4.1134e-006 4.1134e-006 v Velocity[Y] -0.24261 0.89309 0.011097 0.011097 v Velocity[Z] -6.5813e-014 6.2205e-014 -1.127e-016 -1.127e-016 v ǁVelocityǁ 0.00019213 0.8962 0.054396 0.054396 v Pressure -1.0013 1.0064 -7.9936e-016 -3.4694e-016 v TempK 293.9 302.96 296.6 296.6 v Density 1 1 1 1 v CourantNb 0.17955 8 7.4106 7.4106 v FourierNb 0.15798 10 1.3114 1.3114 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3954 21.878 2.8378 2.8378 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.83 303.28 296.62 296.61 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.56554 17.94 8.722 8.722 INSTANT 0.291000000E+02 TIME STEP NUMBER 291 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.54851E-03 0.46532E-01 Friction velocity uk : 0.54851E-03 0.46532E-01 Dimensionless distance yplus : 0.18733E+00 0.15892E+02 Friction thermal sca. tstar : -0.97225E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.13300E+00 0.11283E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.78430E-04 113 0.27475E+00 0.31044E-02 0.74586E+00 c Velocity[X] 0.48378E-03 c Velocity[Y] 0.26206E-02 c Velocity[Z] 0.53418E-29 c Pressure 0.33729E-03 10 0.11045E-07 0.29528E-01 0.99470E-03 c TempK 0.28393E+02 92 0.42928E-03 0.71875E-02 0.22207E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17883 0.1506 1.3922e-005 1.3922e-005 v Velocity[Y] -0.27551 0.84461 0.010917 0.010917 v Velocity[Z] -6.6385e-014 6.6186e-014 -1.3099e-016 -1.3099e-016 v ǁVelocityǁ 3.395e-005 0.84589 0.054266 0.054266 v Pressure -1.0008 1.0068 -7.6383e-016 -2.1684e-016 v TempK 293.93 302.86 296.62 296.62 v Density 1 1 1 1 v CourantNb 0.15829 8 7.4597 7.4597 v FourierNb 0.16864 10 1.2953 1.2953 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35997 21.346 2.8028 2.8028 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.9 303.15 296.64 296.63 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60458 17.138 8.755 8.755 INSTANT 0.292000000E+02 TIME STEP NUMBER 292 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12736E-02 0.48596E-01 Friction velocity uk : 0.12736E-02 0.48596E-01 Dimensionless distance yplus : 0.43498E+00 0.16597E+02 Friction thermal sca. tstar : -0.42265E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.30883E+00 0.11784E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76647E-04 110 0.27891E+00 0.30562E-02 0.75211E+00 c Velocity[X] 0.46302E-03 c Velocity[Y] 0.25932E-02 c Velocity[Z] 0.56116E-29 c Pressure 0.31951E-03 10 0.11639E-07 0.28356E-01 0.92176E-03 c TempK 0.28510E+02 91 0.42943E-03 0.76919E-02 0.23555E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15069 0.16252 9.6991e-006 9.6991e-006 v Velocity[Y] -0.27538 0.84655 0.010914 0.010914 v Velocity[Z] -6.578e-014 6.3777e-014 -1.1973e-016 -1.1973e-016 v ǁVelocityǁ 0.00022942 0.84655 0.054489 0.054489 v Pressure -1.0002 1.0059 -2.4336e-015 -1.8974e-015 v TempK 293.93 302.84 296.63 296.63 v Density 1 1 1 1 v CourantNb 0.16378 8 7.4612 7.4612 v FourierNb 0.17238 10 1.2846 1.2846 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36796 22.668 2.7808 2.7808 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.93 303.15 296.66 296.65 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.91085 17.654 8.7459 8.7459 INSTANT 0.293000000E+02 TIME STEP NUMBER 293 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.83316E-03 0.45865E-01 Friction velocity uk : 0.83316E-03 0.45865E-01 Dimensionless distance yplus : 0.28455E+00 0.15664E+02 Friction thermal sca. tstar : -0.41307E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.20203E+00 0.11121E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76156E-04 111 0.27519E+00 0.29876E-02 0.74700E+00 c Velocity[X] 0.47909E-03 c Velocity[Y] 0.25085E-02 c Velocity[Z] 0.51330E-29 c Pressure 0.32644E-03 11 0.14756E-07 0.31726E-01 0.10933E-02 c TempK 0.28605E+02 88 0.40522E-03 0.65352E-02 0.21222E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18076 0.13113 1.4048e-005 1.4048e-005 v Velocity[Y] -0.2344 0.84643 0.010666 0.010666 v Velocity[Z] -7.079e-014 6.2189e-014 -1.3388e-016 -1.3388e-016 v ǁVelocityǁ 0.00016382 0.85393 0.05447 0.05447 v Pressure -1.0001 1.0079 7.3719e-016 1.301e-015 v TempK 293.92 302.85 296.66 296.66 v Density 1 1 1 1 v CourantNb 0.1308 8 7.559 7.559 v FourierNb 0.17441 10 1.2492 1.2492 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37972 21.346 2.7036 2.7036 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.93 303.15 296.67 296.66 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.539 17.936 8.8081 8.8081 INSTANT 0.294000000E+02 TIME STEP NUMBER 294 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12094E-02 0.49762E-01 Friction velocity uk : 0.12094E-02 0.49762E-01 Dimensionless distance yplus : 0.41304E+00 0.16995E+02 Friction thermal sca. tstar : -0.38038E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.29325E+00 0.12066E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76113E-04 113 0.28243E+00 0.29164E-02 0.72685E+00 c Velocity[X] 0.45444E-03 c Velocity[Y] 0.24620E-02 c Velocity[Z] 0.52855E-29 c Pressure 0.31704E-03 9 0.15244E-07 0.31345E-01 0.10779E-02 c TempK 0.28660E+02 88 0.50671E-03 0.63277E-02 0.21089E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14988 0.15544 3.3626e-006 3.3626e-006 v Velocity[Y] -0.26846 0.86864 0.010902 0.010902 v Velocity[Z] -6.5742e-014 6.1593e-014 -1.3347e-016 -1.3347e-016 v ǁVelocityǁ 0.0010029 0.87037 0.054886 0.054886 v Pressure -0.99984 1.0057 -1.3323e-016 4.6621e-016 v TempK 293.93 302.89 296.67 296.67 v Density 1 1 1 1 v CourantNb 0.45739 8 7.538 7.538 v FourierNb 0.1588 10 1.2379 1.2379 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33896 22.009 2.6799 2.6799 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.92 303.15 296.69 296.68 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69104 18 8.7759 8.7759 INSTANT 0.295000000E+02 TIME STEP NUMBER 295 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.85804E-03 0.45526E-01 Friction velocity uk : 0.85804E-03 0.45526E-01 Dimensionless distance yplus : 0.29305E+00 0.15548E+02 Friction thermal sca. tstar : -0.80613E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.20806E+00 0.11039E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75385E-04 113 0.26211E+00 0.28545E-02 0.70066E+00 c Velocity[X] 0.48609E-03 c Velocity[Y] 0.23684E-02 c Velocity[Z] 0.53389E-29 c Pressure 0.34720E-03 10 0.12929E-07 0.34927E-01 0.98594E-03 c TempK 0.28627E+02 88 0.39143E-03 0.63358E-02 0.21237E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17358 0.16016 9.1966e-006 9.1966e-006 v Velocity[Y] -0.25554 0.91618 0.010857 0.010857 v Velocity[Z] -6.4865e-014 6.5199e-014 -1.4373e-016 -1.4373e-016 v ǁVelocityǁ 0.00026113 0.9185 0.054771 0.054771 v Pressure -0.99975 1.0065 -8.0824e-016 -2.3852e-016 v TempK 293.97 302.91 296.68 296.68 v Density 1 1 1 1 v CourantNb 0.34648 8 7.5518 7.5518 v FourierNb 0.17468 10 1.2201 1.2201 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37286 24.21 2.6424 2.6424 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.93 303.15 296.7 296.7 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75071 16.439 8.7719 8.7719 INSTANT 0.296000000E+02 TIME STEP NUMBER 296 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12184E-03 0.51586E-01 Friction velocity uk : 0.12184E-03 0.51586E-01 Dimensionless distance yplus : 0.41610E-01 0.17618E+02 Friction thermal sca. tstar : -0.15534E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.29543E-01 0.12509E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75603E-04 112 0.26888E+00 0.29519E-02 0.73577E+00 c Velocity[X] 0.50922E-03 c Velocity[Y] 0.24427E-02 c Velocity[Z] 0.49033E-29 c Pressure 0.32708E-03 10 0.16297E-07 0.33431E-01 0.11004E-02 c TempK 0.28584E+02 90 0.41876E-03 0.83727E-02 0.24079E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21422 0.14501 -4.2163e-006 -4.2163e-006 v Velocity[Y] -0.21271 0.85026 0.010666 0.010666 v Velocity[Z] -6.5873e-014 6.8392e-014 -1.2809e-016 -1.2809e-016 v ǁVelocityǁ 0.00022744 0.85074 0.054916 0.054916 v Pressure -0.99973 1.0072 -1.3856e-015 -8.0231e-016 v TempK 294.02 303.02 296.68 296.68 v Density 1 1 1 1 v CourantNb 0.25783 8 7.5195 7.5195 v FourierNb 0.18134 10 1.2173 1.2173 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41014 21.346 2.636 2.636 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 293.97 303.15 296.72 296.71 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73289 17.197 8.7369 8.7369 INSTANT 0.297000000E+02 TIME STEP NUMBER 297 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26793E-03 0.44209E-01 Friction velocity uk : 0.26793E-03 0.44209E-01 Dimensionless distance yplus : 0.91505E-01 0.15099E+02 Friction thermal sca. tstar : -0.88299E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.64967E-01 0.10720E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75250E-04 111 0.26537E+00 0.27807E-02 0.71205E+00 c Velocity[X] 0.44771E-03 c Velocity[Y] 0.23330E-02 c Velocity[Z] 0.52172E-29 c Pressure 0.31957E-03 10 0.15614E-07 0.33726E-01 0.11428E-02 c TempK 0.28509E+02 90 0.45342E-03 0.91446E-02 0.24156E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17796 0.15246 -2.6738e-007 -2.6738e-007 v Velocity[Y] -0.18469 0.88542 0.010701 0.010701 v Velocity[Z] -6.6941e-014 6.7242e-014 -1.1664e-016 -1.1664e-016 v ǁVelocityǁ 9.7668e-005 0.88552 0.054676 0.054676 v Pressure -0.9996 1.0079 -1.9984e-015 -1.4745e-015 v TempK 294.05 303.05 296.69 296.69 v Density 1 1 1 1 v CourantNb 0.22577 8 7.5673 7.5673 v FourierNb 0.1714 10 1.2038 1.2038 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.42787 22.273 2.6072 2.6072 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.02 303.15 296.72 296.71 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.45813 17.582 8.771 8.771 INSTANT 0.298000000E+02 TIME STEP NUMBER 298 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.23476E-03 0.50917E-01 Friction velocity uk : 0.23476E-03 0.50917E-01 Dimensionless distance yplus : 0.80178E-01 0.17390E+02 Friction thermal sca. tstar : -0.83381E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.56925E-01 0.12346E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72496E-04 111 0.25447E+00 0.28769E-02 0.71713E+00 c Velocity[X] 0.43181E-03 c Velocity[Y] 0.24450E-02 c Velocity[Z] 0.47889E-29 c Pressure 0.32136E-03 10 0.13844E-07 0.33016E-01 0.97655E-03 c TempK 0.28393E+02 90 0.43940E-03 0.80565E-02 0.24907E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16712 0.14978 -9.3536e-006 -9.3536e-006 v Velocity[Y] -0.18845 0.85291 0.010799 0.010799 v Velocity[Z] -6.5933e-014 6.4929e-014 -1.3214e-016 -1.3214e-016 v ǁVelocityǁ 0.00060572 0.86115 0.055151 0.055151 v Pressure -0.99953 1.0057 1.5099e-016 8.0231e-016 v TempK 294.05 303.13 296.7 296.7 v Density 1 1 1 1 v CourantNb 0.28091 8 7.5246 7.5246 v FourierNb 0.18128 10 1.2105 1.2105 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38695 22.687 2.6212 2.6212 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.05 303.15 296.73 296.72 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.937 17.234 8.7352 8.7352 INSTANT 0.299000000E+02 TIME STEP NUMBER 299 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.75990E-03 0.47141E-01 Friction velocity uk : 0.75990E-03 0.47141E-01 Dimensionless distance yplus : 0.25953E+00 0.16100E+02 Friction thermal sca. tstar : -0.12236E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.18426E+00 0.11431E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74737E-04 113 0.26937E+00 0.31716E-02 0.75713E+00 c Velocity[X] 0.49479E-03 c Velocity[Y] 0.26769E-02 c Velocity[Z] 0.47909E-29 c Pressure 0.32244E-03 10 0.13576E-07 0.33010E-01 0.10536E-02 c TempK 0.28325E+02 89 0.47463E-03 0.87241E-02 0.24243E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17475 0.14885 2.0306e-005 2.0306e-005 v Velocity[Y] -0.22946 0.81141 0.010606 0.010606 v Velocity[Z] -6.3725e-014 6.754e-014 -1.1871e-016 -1.1871e-016 v ǁVelocityǁ 0.00013045 0.81288 0.05517 0.05517 v Pressure -0.99947 1.0103 -4.2633e-016 9.7578e-017 v TempK 294.03 303.26 296.71 296.71 v Density 1 1 1 1 v CourantNb 0.094327 8 7.5967 7.5967 v FourierNb 0.1686 10 1.2088 1.2088 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.4228 24.956 2.6179 2.6179 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.05 303.15 296.74 296.73 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.29373 17.636 8.8055 8.8055 INSTANT 0.300000000E+02 TIME STEP NUMBER 300 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.61314E-03 0.46889E-01 Friction velocity uk : 0.61314E-03 0.46889E-01 Dimensionless distance yplus : 0.20941E+00 0.16014E+02 Friction thermal sca. tstar : -0.42423E+01 0.19208E+00 Rough dim-less th. sca. tplus : 0.14867E+00 0.11370E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74765E-04 113 0.27350E+00 0.30957E-02 0.77292E+00 c Velocity[X] 0.50688E-03 c Velocity[Y] 0.25888E-02 c Velocity[Z] 0.57637E-29 c Pressure 0.31455E-03 10 0.13675E-07 0.32967E-01 0.10970E-02 c TempK 0.28489E+02 88 0.39818E-03 0.69589E-02 0.23173E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16453 0.16513 6.2303e-007 6.2303e-007 v Velocity[Y] -0.2099 0.86069 0.010519 0.010519 v Velocity[Z] -6.1307e-014 6.557e-014 -1.3733e-016 -1.3733e-016 v ǁVelocityǁ 0.0002911 0.86122 0.054877 0.054877 v Pressure -0.9994 1.0078 8.8818e-017 6.8305e-016 v TempK 294.02 303.35 296.71 296.71 v Density 1 1 1 1 v CourantNb 0.33403 8 7.5856 7.5856 v FourierNb 0.12409 10 1.2028 1.2028 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35317 25.256 2.6051 2.6051 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.03 303.26 296.75 296.74 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.79708 17.984 8.7885 8.7885 INSTANT 0.301000000E+02 TIME STEP NUMBER 301 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28157E-03 0.43499E-01 Friction velocity uk : 0.28157E-03 0.43499E-01 Dimensionless distance yplus : 0.96164E-01 0.14856E+02 Friction thermal sca. tstar : -0.13285E+02 0.30165E+00 Rough dim-less th. sca. tplus : 0.68275E-01 0.10548E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71339E-04 111 0.25067E+00 0.28394E-02 0.71926E+00 c Velocity[X] 0.46165E-03 c Velocity[Y] 0.23778E-02 c Velocity[Z] 0.54619E-29 c Pressure 0.31400E-03 10 0.14822E-07 0.32931E-01 0.10477E-02 c TempK 0.28326E+02 88 0.47274E-03 0.77945E-02 0.23364E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16781 0.21162 1.2318e-005 1.2318e-005 v Velocity[Y] -0.21127 0.82631 0.0106 0.0106 v Velocity[Z] -5.9353e-014 7.2374e-014 -1.1355e-016 -1.1355e-016 v ǁVelocityǁ 0.0004169 0.82981 0.05467 0.05467 v Pressure -0.99934 1.0089 -1.6342e-015 -1.0517e-015 v TempK 294.06 303.54 296.71 296.71 v Density 1 1 1 1 v CourantNb 0.4625 8 7.5413 7.5413 v FourierNb 0.1365 9.4962 1.1997 1.1997 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38849 25.311 2.5958 2.5958 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.02 303.35 296.75 296.74 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73956 16.843 8.741 8.741 INSTANT 0.302000000E+02 TIME STEP NUMBER 302 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12073E-02 0.47594E-01 Friction velocity uk : 0.12073E-02 0.47594E-01 Dimensionless distance yplus : 0.41232E+00 0.16255E+02 Friction thermal sca. tstar : -0.68645E+01 0.74000E+00 Rough dim-less th. sca. tplus : 0.29274E+00 0.11541E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73554E-04 112 0.25639E+00 0.29247E-02 0.72887E+00 c Velocity[X] 0.49778E-03 c Velocity[Y] 0.24269E-02 c Velocity[Z] 0.45581E-29 c Pressure 0.33510E-03 9 0.14782E-07 0.34876E-01 0.10171E-02 c TempK 0.28232E+02 88 0.42137E-03 0.56401E-02 0.21912E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17368 0.19469 -3.2557e-006 -3.2557e-006 v Velocity[Y] -0.20111 0.93268 0.010524 0.010524 v Velocity[Z] -6.7096e-014 6.8997e-014 -1.3137e-016 -1.3137e-016 v ǁVelocityǁ 0.00023884 0.93281 0.054776 0.054776 v Pressure -0.99931 1.0054 -1.1546e-016 4.12e-016 v TempK 294.12 303.68 296.72 296.72 v Density 1 1 1 1 v CourantNb 0.39567 8 7.5183 7.5183 v FourierNb 0.15015 9.9293 1.2024 1.2024 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38488 21.928 2.599 2.599 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.06 303.54 296.74 296.74 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.65411 17.929 8.7208 8.7208 INSTANT 0.303000000E+02 TIME STEP NUMBER 303 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.99794E-03 0.44554E-01 Friction velocity uk : 0.99794E-03 0.44554E-01 Dimensionless distance yplus : 0.34083E+00 0.15217E+02 Friction thermal sca. tstar : -0.70825E+01 0.72422E+00 Rough dim-less th. sca. tplus : 0.24198E+00 0.10804E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72912E-04 114 0.27455E+00 0.28917E-02 0.73701E+00 c Velocity[X] 0.47589E-03 c Velocity[Y] 0.24158E-02 c Velocity[Z] 0.53513E-29 c Pressure 0.30883E-03 9 0.13260E-07 0.31583E-01 0.10270E-02 c TempK 0.28278E+02 88 0.41323E-03 0.68472E-02 0.21327E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17052 0.11996 8.0228e-006 8.0228e-006 v Velocity[Y] -0.18818 0.96329 0.010555 0.010555 v Velocity[Z] -6.1608e-014 6.9827e-014 -1.2898e-016 -1.2898e-016 v ǁVelocityǁ 0.00035911 0.96333 0.054189 0.054189 v Pressure -0.99926 1.0072 -8.1712e-016 -2.6021e-016 v TempK 294.18 303.79 296.72 296.72 v Density 1 1 1 1 v CourantNb 0.19826 8 7.4945 7.4945 v FourierNb 0.16517 9.917 1.2156 1.2156 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38677 23.335 2.6284 2.6284 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.12 303.68 296.76 296.75 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60757 17.917 8.7101 8.7101 INSTANT 0.304000000E+02 TIME STEP NUMBER 304 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.77757E-03 0.53108E-01 Friction velocity uk : 0.77757E-03 0.53108E-01 Dimensionless distance yplus : 0.26557E+00 0.18138E+02 Friction thermal sca. tstar : -0.53199E+01 0.11798E+01 Rough dim-less th. sca. tplus : 0.18855E+00 0.12878E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71096E-04 112 0.27051E+00 0.27671E-02 0.70336E+00 c Velocity[X] 0.45215E-03 c Velocity[Y] 0.23149E-02 c Velocity[Z] 0.55434E-29 c Pressure 0.33663E-03 10 0.14160E-07 0.33822E-01 0.10649E-02 c TempK 0.28183E+02 87 0.36388E-03 0.48769E-02 0.18900E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17416 0.14145 -6.3901e-006 -6.3901e-006 v Velocity[Y] -0.19326 0.86582 0.010782 0.010782 v Velocity[Z] -6.1329e-014 6.7463e-014 -1.1349e-016 -1.1349e-016 v ǁVelocityǁ 0.00032885 0.86612 0.054156 0.054156 v Pressure -0.99921 1.0063 -2.2204e-016 3.361e-016 v TempK 294.19 303.86 296.72 296.72 v Density 1 1 1 1 v CourantNb 0.36769 8 7.4214 7.4214 v FourierNb 0.16136 10 1.2307 1.2307 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39456 21.346 2.6604 2.6604 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.18 303.79 296.76 296.75 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.79179 17.751 8.652 8.652 INSTANT 0.305000000E+02 TIME STEP NUMBER 305 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.40048E-03 0.43487E-01 Friction velocity uk : 0.40048E-03 0.43487E-01 Dimensionless distance yplus : 0.13678E+00 0.14852E+02 Friction thermal sca. tstar : -0.85029E+01 0.34421E+01 Rough dim-less th. sca. tplus : 0.97109E-01 0.10545E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72971E-04 112 0.27120E+00 0.28380E-02 0.71035E+00 c Velocity[X] 0.52249E-03 c Velocity[Y] 0.23155E-02 c Velocity[Z] 0.48676E-29 c Pressure 0.33216E-03 10 0.12719E-07 0.32575E-01 0.10860E-02 c TempK 0.27965E+02 88 0.42827E-03 0.45123E-02 0.17911E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19755 0.14711 6.5293e-006 6.5293e-006 v Velocity[Y] -0.20493 0.81936 0.010721 0.010721 v Velocity[Z] -6.0752e-014 6.8046e-014 -1.0279e-016 -1.0279e-016 v ǁVelocityǁ 0.00019466 0.82351 0.054215 0.054215 v Pressure -0.99923 1.0079 -5.0626e-016 9.7578e-017 v TempK 294.17 303.87 296.71 296.71 v Density 1 1 1 1 v CourantNb 0.37799 8 7.4666 7.4666 v FourierNb 0.17749 10 1.2532 1.2532 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40684 21.346 2.7102 2.7102 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.19 303.86 296.75 296.75 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72083 17.705 8.7198 8.7198 INSTANT 0.306000000E+02 TIME STEP NUMBER 306 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14882E-03 0.48010E-01 Friction velocity uk : 0.14882E-03 0.48010E-01 Dimensionless distance yplus : 0.50826E-01 0.16397E+02 Friction thermal sca. tstar : -0.61999E+01 0.93220E+00 Rough dim-less th. sca. tplus : 0.36085E-01 0.11642E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71872E-04 110 0.26428E+00 0.28421E-02 0.72262E+00 c Velocity[X] 0.50799E-03 c Velocity[Y] 0.23341E-02 c Velocity[Z] 0.48094E-29 c Pressure 0.32814E-03 10 0.12216E-07 0.30650E-01 0.10704E-02 c TempK 0.27822E+02 88 0.34039E-03 0.38514E-02 0.18067E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14318 0.15905 5.6746e-006 5.6746e-006 v Velocity[Y] -0.18221 0.87495 0.010647 0.010647 v Velocity[Z] -5.9872e-014 6.378e-014 -1.3086e-016 -1.3086e-016 v ǁVelocityǁ 0.00049999 0.87574 0.053892 0.053892 v Pressure -0.99935 1.0069 8.8818e-016 1.507e-015 v TempK 294.15 303.98 296.72 296.72 v Density 1 1 1 1 v CourantNb 0.26568 8 7.507 7.507 v FourierNb 0.18618 10 1.2618 1.2618 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40189 21.346 2.7288 2.7288 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.17 303.87 296.75 296.75 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.59111 17.435 8.7688 8.7688 INSTANT 0.307000000E+02 TIME STEP NUMBER 307 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.77972E-03 0.44114E-01 Friction velocity uk : 0.77972E-03 0.44114E-01 Dimensionless distance yplus : 0.26630E+00 0.15066E+02 Friction thermal sca. tstar : -0.81342E+01 0.13451E+01 Rough dim-less th. sca. tplus : 0.18907E+00 0.10697E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73348E-04 113 0.27894E+00 0.26378E-02 0.69381E+00 c Velocity[X] 0.44280E-03 c Velocity[Y] 0.21950E-02 c Velocity[Z] 0.47774E-29 c Pressure 0.33161E-03 10 0.11999E-07 0.29865E-01 0.10753E-02 c TempK 0.27611E+02 89 0.42055E-03 0.44613E-02 0.17610E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16871 0.13784 9.4394e-006 9.4394e-006 v Velocity[Y] -0.18499 0.84809 0.010655 0.010655 v Velocity[Z] -6.4818e-014 6.0977e-014 -1.4702e-016 -1.4702e-016 v ǁVelocityǁ 0.00034819 0.8482 0.053516 0.053516 v Pressure -0.99981 1.0079 -6.2172e-017 4.9873e-016 v TempK 294.16 304.13 296.73 296.73 v Density 1 1 1 1 v CourantNb 0.46304 8 7.4951 7.4951 v FourierNb 0.18069 10 1.2803 1.2803 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39949 21.346 2.7701 2.7701 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.15 303.98 296.76 296.75 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.9065 17.623 8.7755 8.7755 INSTANT 0.308000000E+02 TIME STEP NUMBER 308 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.88104E-03 0.49337E-01 Friction velocity uk : 0.88104E-03 0.49337E-01 Dimensionless distance yplus : 0.30090E+00 0.16850E+02 Friction thermal sca. tstar : -0.44005E+01 0.45917E+01 Rough dim-less th. sca. tplus : 0.21364E+00 0.11963E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69516E-04 111 0.26581E+00 0.25851E-02 0.66604E+00 c Velocity[X] 0.43767E-03 c Velocity[Y] 0.21475E-02 c Velocity[Z] 0.43541E-29 c Pressure 0.33488E-03 10 0.11857E-07 0.28156E-01 0.10571E-02 c TempK 0.27446E+02 88 0.41961E-03 0.43040E-02 0.18269E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18475 0.18986 -3.391e-006 -3.391e-006 v Velocity[Y] -0.17102 1.0022 0.010883 0.010883 v Velocity[Z] -6.3187e-014 5.9874e-014 -1.3761e-016 -1.3761e-016 v ǁVelocityǁ 0.00041232 1.0098 0.053397 0.053397 v Pressure -1.0001 1.0055 -3.1974e-016 1.7347e-016 v TempK 294.2 304.21 296.73 296.73 v Density 1 1 1 1 v CourantNb 0.24499 8 7.4649 7.4649 v FourierNb 0.17453 10 1.3078 1.3078 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41463 22.077 2.8306 2.8306 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.16 304.13 296.77 296.76 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72751 17.362 8.7727 8.7727 INSTANT 0.309000000E+02 TIME STEP NUMBER 309 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10730E-02 0.44946E-01 Friction velocity uk : 0.10730E-02 0.44946E-01 Dimensionless distance yplus : 0.36645E+00 0.15350E+02 Friction thermal sca. tstar : -0.43703E+01 0.16615E+01 Rough dim-less th. sca. tplus : 0.26017E+00 0.10899E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69908E-04 112 0.26580E+00 0.26678E-02 0.68500E+00 c Velocity[X] 0.46428E-03 c Velocity[Y] 0.22036E-02 c Velocity[Z] 0.42320E-29 c Pressure 0.33844E-03 10 0.13077E-07 0.28377E-01 0.11453E-02 c TempK 0.27337E+02 88 0.43669E-03 0.32332E-02 0.16091E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1676 0.14043 1.5733e-005 1.5733e-005 v Velocity[Y] -0.24205 0.90267 0.010886 0.010886 v Velocity[Z] -5.9129e-014 6.523e-014 -1.1812e-016 -1.1812e-016 v ǁVelocityǁ 6.1215e-005 0.90313 0.053193 0.053193 v Pressure -1.0006 1.0098 -2.7534e-016 3.2526e-016 v TempK 294.25 304.21 296.74 296.74 v Density 1 1 1 1 v CourantNb 0.28782 8 7.4912 7.4912 v FourierNb 0.16903 10 1.3318 1.3318 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.43377 23.067 2.8808 2.8808 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.2 304.21 296.77 296.76 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.64252 17.714 8.823 8.823 INSTANT 0.310000000E+02 TIME STEP NUMBER 310 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.70752E-03 0.51410E-01 Friction velocity uk : 0.70752E-03 0.51410E-01 Dimensionless distance yplus : 0.24164E+00 0.17558E+02 Friction thermal sca. tstar : -0.41189E+01 0.11634E+01 Rough dim-less th. sca. tplus : 0.17156E+00 0.12466E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.68640E-04 113 0.27596E+00 0.25856E-02 0.66306E+00 c Velocity[X] 0.44015E-03 c Velocity[Y] 0.21455E-02 c Velocity[Z] 0.47810E-29 c Pressure 0.31272E-03 10 0.13118E-07 0.25548E-01 0.10544E-02 c TempK 0.27253E+02 89 0.36533E-03 0.39646E-02 0.17868E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16788 0.15777 1.9718e-006 1.9718e-006 v Velocity[Y] -0.16501 0.91074 0.011 0.011 v Velocity[Z] -6.2803e-014 5.9506e-014 -1.4111e-016 -1.4111e-016 v ǁVelocityǁ 0.00065754 0.91081 0.053311 0.053311 v Pressure -1.001 1.005 -1.0836e-015 -5.5294e-016 v TempK 294.28 304.08 296.75 296.75 v Density 1 1 1 1 v CourantNb 0.376 8 7.4821 7.4821 v FourierNb 0.165 10 1.3596 1.3596 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41722 25.373 2.9425 2.9425 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.25 304.21 296.78 296.77 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.2419 17.729 8.8417 8.8417 INSTANT 0.311000000E+02 TIME STEP NUMBER 311 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.50437E-03 0.45448E-01 Friction velocity uk : 0.50437E-03 0.45448E-01 Dimensionless distance yplus : 0.17226E+00 0.15522E+02 Friction thermal sca. tstar : -0.86138E+01 0.93023E+00 Rough dim-less th. sca. tplus : 0.12230E+00 0.11020E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72482E-04 111 0.27823E+00 0.27244E-02 0.68368E+00 c Velocity[X] 0.43625E-03 c Velocity[Y] 0.22882E-02 c Velocity[Z] 0.51355E-29 c Pressure 0.32430E-03 10 0.14735E-07 0.26953E-01 0.95676E-03 c TempK 0.27311E+02 90 0.48928E-03 0.44265E-02 0.18620E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1584 0.18903 7.3993e-006 7.3993e-006 v Velocity[Y] -0.22576 0.92669 0.011037 0.011037 v Velocity[Z] -6.4603e-014 6.3701e-014 -1.3145e-016 -1.3145e-016 v ǁVelocityǁ 0.00015358 0.9295 0.053309 0.053309 v Pressure -1.0012 1.0087 -9.77e-016 -4.6621e-016 v TempK 294.3 304.05 296.77 296.77 v Density 1 1 1 1 v CourantNb 0.43995 8 7.5131 7.5131 v FourierNb 0.18149 10 1.339 1.339 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39877 25.92 2.8998 2.8998 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.28 304.08 296.79 296.78 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.92125 17.408 8.8521 8.8521 INSTANT 0.312000000E+02 TIME STEP NUMBER 312 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.77450E-03 0.50732E-01 Friction velocity uk : 0.77450E-03 0.50732E-01 Dimensionless distance yplus : 0.26452E+00 0.17327E+02 Friction thermal sca. tstar : -0.67840E+01 0.48038E+01 Rough dim-less th. sca. tplus : 0.18780E+00 0.12302E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73471E-04 112 0.29206E+00 0.28857E-02 0.72611E+00 c Velocity[X] 0.45428E-03 c Velocity[Y] 0.24315E-02 c Velocity[Z] 0.41970E-29 c Pressure 0.32003E-03 10 0.11054E-07 0.26700E-01 0.96100E-03 c TempK 0.27344E+02 90 0.43738E-03 0.47559E-02 0.22392E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1833 0.17346 -1.0576e-005 -1.0576e-005 v Velocity[Y] -0.17735 0.9136 0.010946 0.010946 v Velocity[Z] -6.5249e-014 6.418e-014 -1.5346e-016 -1.5346e-016 v ǁVelocityǁ 5.8373e-006 0.91497 0.052917 0.052917 v Pressure -1.0011 1.0058 3.5527e-017 5.9631e-016 v TempK 294.31 304.08 296.78 296.78 v Density 1 1 1 1 v CourantNb 0.37224 8 7.5247 7.5247 v FourierNb 0.15805 10 1.3509 1.3509 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33736 28.461 2.9259 2.9259 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.3 304.05 296.81 296.8 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73567 17.603 8.8757 8.8757 INSTANT 0.313000000E+02 TIME STEP NUMBER 313 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.67930E-03 0.45232E-01 Friction velocity uk : 0.67930E-03 0.45232E-01 Dimensionless distance yplus : 0.23200E+00 0.15448E+02 Friction thermal sca. tstar : -0.69915E+01 0.12626E+01 Rough dim-less th. sca. tplus : 0.16472E+00 0.10968E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72623E-04 110 0.25858E+00 0.27847E-02 0.69808E+00 c Velocity[X] 0.48885E-03 c Velocity[Y] 0.22959E-02 c Velocity[Z] 0.47972E-29 c Pressure 0.31927E-03 10 0.99869E-08 0.25336E-01 0.10203E-02 c TempK 0.27286E+02 89 0.43771E-03 0.47969E-02 0.19869E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1573 0.16421 1.0536e-005 1.0536e-005 v Velocity[Y] -0.18243 0.93778 0.010828 0.010828 v Velocity[Z] -6.4495e-014 6.3196e-014 -1.4929e-016 -1.4929e-016 v ǁVelocityǁ 0.00037941 0.93932 0.052844 0.052844 v Pressure -1.0005 1.0112 4.5297e-016 9.6494e-016 v TempK 294.32 303.99 296.79 296.79 v Density 1 1 1 1 v CourantNb 0.2671 8 7.4769 7.4769 v FourierNb 0.17385 10 1.3639 1.3639 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3711 28.461 2.9513 2.9513 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.31 304.08 296.82 296.81 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.54065 17.771 8.8408 8.8408 INSTANT 0.314000000E+02 TIME STEP NUMBER 314 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.97920E-03 0.46246E-01 Friction velocity uk : 0.97920E-03 0.46246E-01 Dimensionless distance yplus : 0.33443E+00 0.15794E+02 Friction thermal sca. tstar : -0.45710E+01 0.86716E+00 Rough dim-less th. sca. tplus : 0.23744E+00 0.11214E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74779E-04 113 0.26268E+00 0.28580E-02 0.72280E+00 c Velocity[X] 0.50777E-03 c Velocity[Y] 0.23503E-02 c Velocity[Z] 0.47437E-29 c Pressure 0.32605E-03 10 0.10980E-07 0.26265E-01 0.10023E-02 c TempK 0.27360E+02 89 0.45626E-03 0.43749E-02 0.19055E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20778 0.13911 9.5015e-006 9.5015e-006 v Velocity[Y] -0.22884 0.7858 0.010765 0.010765 v Velocity[Z] -6.4292e-014 6.5814e-014 -1.348e-016 -1.348e-016 v ǁVelocityǁ 0.00047397 0.78635 0.05293 0.05293 v Pressure -0.99985 1.0056 -1.3234e-015 -8.1315e-016 v TempK 294.37 303.84 296.8 296.8 v Density 1 1 1 1 v CourantNb 0.42001 8 7.5147 7.5147 v FourierNb 0.15497 10 1.3663 1.3663 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40159 25.624 2.955 2.955 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.32 303.99 296.83 296.82 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0219 17.958 8.881 8.881 INSTANT 0.315000000E+02 TIME STEP NUMBER 315 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.87055E-03 0.44526E-01 Friction velocity uk : 0.87055E-03 0.44526E-01 Dimensionless distance yplus : 0.29732E+00 0.15207E+02 Friction thermal sca. tstar : -0.42106E+01 0.59680E+00 Rough dim-less th. sca. tplus : 0.21109E+00 0.10797E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72781E-04 111 0.28113E+00 0.29117E-02 0.73793E+00 c Velocity[X] 0.47019E-03 c Velocity[Y] 0.24415E-02 c Velocity[Z] 0.46071E-29 c Pressure 0.30322E-03 10 0.10496E-07 0.23115E-01 0.99374E-03 c TempK 0.27542E+02 88 0.51331E-03 0.54390E-02 0.20782E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16681 0.15663 1.7671e-005 1.7671e-005 v Velocity[Y] -0.22425 0.8313 0.01069 0.01069 v Velocity[Z] -6.1486e-014 6.6364e-014 -1.138e-016 -1.138e-016 v ǁVelocityǁ 0.00012706 0.83333 0.052354 0.052354 v Pressure -0.99992 1.0079 -6.4837e-016 -6.5052e-017 v TempK 294.43 303.65 296.8 296.8 v Density 1 1 1 1 v CourantNb 0.27104 8 7.5281 7.5281 v FourierNb 0.17047 10 1.3862 1.3862 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.43296 23.672 2.999 2.999 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.37 303.84 296.83 296.83 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81337 17.856 8.9144 8.9144 INSTANT 0.316000000E+02 TIME STEP NUMBER 316 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.64170E-03 0.48483E-01 Friction velocity uk : 0.64170E-03 0.48483E-01 Dimensionless distance yplus : 0.21916E+00 0.16558E+02 Friction thermal sca. tstar : -0.61205E+01 0.43102E+00 Rough dim-less th. sca. tplus : 0.15560E+00 0.11756E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70617E-04 109 0.26444E+00 0.27581E-02 0.69729E+00 c Velocity[X] 0.44115E-03 c Velocity[Y] 0.23169E-02 c Velocity[Z] 0.48316E-29 c Pressure 0.31961E-03 9 0.10956E-07 0.23261E-01 0.95166E-03 c TempK 0.27545E+02 88 0.37836E-03 0.54227E-02 0.21341E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17281 0.16006 8.1993e-006 8.1993e-006 v Velocity[Y] -0.25539 0.91609 0.010864 0.010864 v Velocity[Z] -6.3797e-014 6.3851e-014 -1.414e-016 -1.414e-016 v ǁVelocityǁ 0.00022003 0.91609 0.052454 0.052454 v Pressure -0.99972 1.0066 -7.0166e-016 -3.2526e-017 v TempK 294.49 303.45 296.81 296.81 v Density 1 1 1 1 v CourantNb 0.3538 8 7.4513 7.4513 v FourierNb 0.18366 10 1.411 1.411 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.43856 26.039 3.0547 3.0547 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.43 303.65 296.84 296.83 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.74494 17.086 8.8623 8.8623 INSTANT 0.317000000E+02 TIME STEP NUMBER 317 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.22262E-03 0.43587E-01 Friction velocity uk : 0.22262E-03 0.43587E-01 Dimensionless distance yplus : 0.76030E-01 0.14886E+02 Friction thermal sca. tstar : -0.28631E+02 0.58062E+00 Rough dim-less th. sca. tplus : 0.53980E-01 0.10569E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73233E-04 111 0.27178E+00 0.29318E-02 0.73508E+00 c Velocity[X] 0.50081E-03 c Velocity[Y] 0.24310E-02 c Velocity[Z] 0.45131E-29 c Pressure 0.34437E-03 10 0.10116E-07 0.25399E-01 0.10540E-02 c TempK 0.27557E+02 88 0.42434E-03 0.43927E-02 0.19066E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16889 0.19381 2.8055e-005 2.8055e-005 v Velocity[Y] -0.28148 0.84489 0.010894 0.010894 v Velocity[Z] -6.364e-014 6.0185e-014 -1.305e-016 -1.305e-016 v ǁVelocityǁ 0.00034316 0.84576 0.052654 0.052654 v Pressure -0.99972 1.01 -1.6254e-015 -9.6494e-016 v TempK 294.54 303.39 296.82 296.82 v Density 1 1 1 1 v CourantNb 0.2192 8 7.4696 7.4696 v FourierNb 0.14907 10 1.4221 1.4221 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.347 28.461 3.0811 3.0811 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.49 303.45 296.85 296.84 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.8965 17.673 8.8917 8.8917 INSTANT 0.318000000E+02 TIME STEP NUMBER 318 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.48056E-03 0.45689E-01 Friction velocity uk : 0.48056E-03 0.45689E-01 Dimensionless distance yplus : 0.16412E+00 0.15604E+02 Friction thermal sca. tstar : -0.74632E+01 0.12782E+01 Rough dim-less th. sca. tplus : 0.11653E+00 0.11079E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74892E-04 111 0.26769E+00 0.30192E-02 0.74231E+00 c Velocity[X] 0.51629E-03 c Velocity[Y] 0.25029E-02 c Velocity[Z] 0.54826E-29 c Pressure 0.33158E-03 10 0.10646E-07 0.23643E-01 0.10900E-02 c TempK 0.27635E+02 88 0.39751E-03 0.44740E-02 0.18315E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16941 0.17049 1.4063e-005 1.4063e-005 v Velocity[Y] -0.24912 0.85631 0.010612 0.010612 v Velocity[Z] -6.352e-014 5.9091e-014 -1.2121e-016 -1.2121e-016 v ǁVelocityǁ 0.00039902 0.85657 0.052211 0.052211 v Pressure -0.99976 1.006 -1.7053e-015 -1.1493e-015 v TempK 294.58 303.27 296.84 296.84 v Density 1 1 1 1 v CourantNb 0.32082 8 7.4762 7.4762 v FourierNb 0.16397 10 1.4405 1.4405 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3817 28.461 3.1209 3.1209 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.54 303.39 296.86 296.85 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.62062 17.937 8.9167 8.9167 INSTANT 0.319000000E+02 TIME STEP NUMBER 319 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.31050E-03 0.42595E-01 Friction velocity uk : 0.31050E-03 0.42595E-01 Dimensionless distance yplus : 0.10605E+00 0.14547E+02 Friction thermal sca. tstar : -0.53581E+01 0.26290E+00 Rough dim-less th. sca. tplus : 0.75291E-01 0.10328E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74290E-04 110 0.27226E+00 0.28785E-02 0.73502E+00 c Velocity[X] 0.45603E-03 c Velocity[Y] 0.24225E-02 c Velocity[Z] 0.48119E-29 c Pressure 0.31870E-03 9 0.10419E-07 0.23755E-01 0.10762E-02 c TempK 0.27628E+02 88 0.38155E-03 0.46497E-02 0.18137E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17486 0.14693 1.825e-005 1.825e-005 v Velocity[Y] -0.23265 0.8908 0.010679 0.010679 v Velocity[Z] -6.5271e-014 6.0258e-014 -1.2869e-016 -1.2869e-016 v ǁVelocityǁ 7.4808e-005 0.89232 0.051974 0.051974 v Pressure -0.99971 1.0073 -1.7053e-015 -1.1167e-015 v TempK 294.61 303.11 296.85 296.85 v Density 1 1 1 1 v CourantNb 0.13451 8 7.4633 7.4633 v FourierNb 0.18037 10 1.4291 1.4291 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40103 28.461 3.0978 3.0978 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.58 303.27 296.88 296.87 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.71123 17.944 8.8924 8.8924 INSTANT 0.320000000E+02 TIME STEP NUMBER 320 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.27777E-03 0.49201E-01 Friction velocity uk : 0.27777E-03 0.49201E-01 Dimensionless distance yplus : 0.94866E-01 0.16804E+02 Friction thermal sca. tstar : -0.58229E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.67353E-01 0.11930E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76027E-04 113 0.27299E+00 0.29520E-02 0.74946E+00 c Velocity[X] 0.46912E-03 c Velocity[Y] 0.24829E-02 c Velocity[Z] 0.43467E-29 c Pressure 0.33010E-03 10 0.10003E-07 0.25467E-01 0.11010E-02 c TempK 0.27558E+02 89 0.40430E-03 0.44736E-02 0.17215E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16198 0.1745 7.4209e-006 7.4209e-006 v Velocity[Y] -0.28024 0.92716 0.010644 0.010644 v Velocity[Z] -6.5251e-014 5.8485e-014 -1.3913e-016 -1.3913e-016 v ǁVelocityǁ 0.00012837 0.92716 0.051921 0.051921 v Pressure -1.0001 1.0062 -6.3949e-016 3.2526e-017 v TempK 294.65 302.98 296.86 296.86 v Density 1 1 1 1 v CourantNb 0.52097 8 7.4707 7.4707 v FourierNb 0.1277 10 1.4351 1.4351 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35809 28.461 3.1097 3.1097 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.61 303.15 296.89 296.88 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.3742 17.832 8.9058 8.9058 INSTANT 0.321000000E+02 TIME STEP NUMBER 321 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.36602E-03 0.46683E-01 Friction velocity uk : 0.36602E-03 0.46683E-01 Dimensionless distance yplus : 0.12501E+00 0.15944E+02 Friction thermal sca. tstar : -0.15368E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.88754E-01 0.11320E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76537E-04 110 0.27626E+00 0.28894E-02 0.73116E+00 c Velocity[X] 0.47347E-03 c Velocity[Y] 0.24159E-02 c Velocity[Z] 0.48522E-29 c Pressure 0.32504E-03 9 0.13288E-07 0.25381E-01 0.10614E-02 c TempK 0.27559E+02 90 0.39091E-03 0.54705E-02 0.17722E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14672 0.15531 2.8601e-005 2.8601e-005 v Velocity[Y] -0.28593 1.025 0.010681 0.010681 v Velocity[Z] -6.4222e-014 5.8318e-014 -1.3445e-016 -1.3445e-016 v ǁVelocityǁ 0.00017221 1.025 0.051692 0.051692 v Pressure -1.0001 1.0086 -1.2612e-015 -6.5052e-016 v TempK 294.73 302.93 296.88 296.88 v Density 1 1 1 1 v CourantNb 0.48176 8 7.4227 7.4227 v FourierNb 0.14047 10 1.446 1.446 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37989 28.461 3.1349 3.1349 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.65 303.15 296.9 296.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.97226 17.884 8.8687 8.8687 INSTANT 0.322000000E+02 TIME STEP NUMBER 322 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.37763E-03 0.52910E-01 Friction velocity uk : 0.37763E-03 0.52910E-01 Dimensionless distance yplus : 0.12897E+00 0.18070E+02 Friction thermal sca. tstar : -0.44985E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.91568E-01 0.12830E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74516E-04 111 0.27106E+00 0.29596E-02 0.74348E+00 c Velocity[X] 0.47085E-03 c Velocity[Y] 0.24887E-02 c Velocity[Z] 0.50449E-29 c Pressure 0.32536E-03 10 0.13135E-07 0.25621E-01 0.11651E-02 c TempK 0.27500E+02 89 0.36264E-03 0.60671E-02 0.20364E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16538 0.16114 1.0542e-006 1.0542e-006 v Velocity[Y] -0.25085 0.95314 0.010766 0.010766 v Velocity[Z] -6.1843e-014 6.1527e-014 -1.2634e-016 -1.2634e-016 v ǁVelocityǁ 0.00016854 0.95645 0.051546 0.051546 v Pressure -1.0001 1.0057 -1.4744e-015 -8.6736e-016 v TempK 294.82 302.85 296.88 296.88 v Density 1 1 1 1 v CourantNb 0.11189 8 7.4413 7.4413 v FourierNb 0.15022 10 1.4559 1.4559 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38214 28.461 3.1558 3.1558 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.73 303.15 296.91 296.91 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69669 17.731 8.8972 8.8972 INSTANT 0.323000000E+02 TIME STEP NUMBER 323 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.35617E-03 0.40412E-01 Friction velocity uk : 0.35617E-03 0.40412E-01 Dimensionless distance yplus : 0.12164E+00 0.13802E+02 Friction thermal sca. tstar : -0.30659E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.86365E-01 0.97991E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75492E-04 110 0.26934E+00 0.28889E-02 0.72627E+00 c Velocity[X] 0.47681E-03 c Velocity[Y] 0.24121E-02 c Velocity[Z] 0.47332E-29 c Pressure 0.32515E-03 10 0.99537E-08 0.24891E-01 0.93984E-03 c TempK 0.27467E+02 91 0.46760E-03 0.11342E-01 0.25826E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1495 0.1996 6.3562e-006 6.3562e-006 v Velocity[Y] -0.23193 0.89305 0.01071 0.01071 v Velocity[Z] -6.2554e-014 6.3851e-014 -1.2447e-016 -1.2447e-016 v ǁVelocityǁ 0.00028338 0.89357 0.051665 0.051665 v Pressure -1.0004 1.0078 -1.5721e-015 -9.541e-016 v TempK 294.9 302.88 296.91 296.91 v Density 1 1 1 1 v CourantNb 0.21924 8 7.4152 7.4152 v FourierNb 0.16524 10 1.4543 1.4543 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40711 21.346 3.1488 3.1488 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.82 303.15 296.92 296.91 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60826 17.833 8.8695 8.8695 INSTANT 0.324000000E+02 TIME STEP NUMBER 324 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.41275E-03 0.49969E-01 Friction velocity uk : 0.41275E-03 0.49969E-01 Dimensionless distance yplus : 0.14097E+00 0.17066E+02 Friction thermal sca. tstar : -0.40318E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.10008E+00 0.12116E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76099E-04 116 0.26154E+00 0.31099E-02 0.77823E+00 c Velocity[X] 0.47238E-03 c Velocity[Y] 0.26375E-02 c Velocity[Z] 0.47518E-29 c Pressure 0.32800E-03 10 0.12245E-07 0.24946E-01 0.95125E-03 c TempK 0.27546E+02 90 0.46766E-03 0.11061E-01 0.24762E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1809 0.19665 -1.8945e-005 -1.8945e-005 v Velocity[Y] -0.24203 0.90568 0.01064 0.01064 v Velocity[Z] -6.1855e-014 7.1344e-014 -1.463e-016 -1.463e-016 v ǁVelocityǁ 0.00010473 0.90661 0.051806 0.051806 v Pressure -1.0007 1.0062 -1.2434e-016 3.9031e-016 v TempK 294.96 302.89 296.94 296.94 v Density 1 1 1 1 v CourantNb 0.30103 8 7.4961 7.4961 v FourierNb 0.13756 10 1.4451 1.4451 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32201 23.21 3.1301 3.1301 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.9 303.15 296.95 296.94 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.54785 17.778 8.9413 8.9413 INSTANT 0.325000000E+02 TIME STEP NUMBER 325 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11976E-02 0.41510E-01 Friction velocity uk : 0.11976E-02 0.41510E-01 Dimensionless distance yplus : 0.40901E+00 0.14177E+02 Friction thermal sca. tstar : -0.55596E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.29039E+00 0.10065E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75270E-04 113 0.27400E+00 0.30468E-02 0.76012E+00 c Velocity[X] 0.46640E-03 c Velocity[Y] 0.25804E-02 c Velocity[Z] 0.46237E-29 c Pressure 0.32038E-03 10 0.10138E-07 0.24131E-01 0.98801E-03 c TempK 0.27669E+02 91 0.56496E-03 0.12107E-01 0.27484E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.176 0.14924 1.7841e-005 1.7841e-005 v Velocity[Y] -0.23256 0.86222 0.010659 0.010659 v Velocity[Z] -5.8196e-014 6.8679e-014 -1.2405e-016 -1.2405e-016 v ǁVelocityǁ 0.00061961 0.86908 0.051784 0.051784 v Pressure -1.0008 1.0055 1.0481e-015 1.5938e-015 v TempK 294.99 302.87 296.95 296.95 v Density 1 1 1 1 v CourantNb 0.06452 8 7.4953 7.4953 v FourierNb 0.15132 10 1.4329 1.4329 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35422 25.531 3.1048 3.1048 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.96 303.15 296.97 296.97 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.49968 17.604 8.9282 8.9282 INSTANT 0.326000000E+02 TIME STEP NUMBER 326 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.43725E-03 0.47111E-01 Friction velocity uk : 0.43725E-03 0.47111E-01 Dimensionless distance yplus : 0.14934E+00 0.16090E+02 Friction thermal sca. tstar : -0.66073E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.10603E+00 0.11423E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75651E-04 112 0.26465E+00 0.29875E-02 0.74174E+00 c Velocity[X] 0.46767E-03 c Velocity[Y] 0.25198E-02 c Velocity[Z] 0.50218E-29 c Pressure 0.32092E-03 10 0.10171E-07 0.23364E-01 0.10077E-02 c TempK 0.27676E+02 91 0.53454E-03 0.13452E-01 0.29776E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14312 0.17989 -1.5285e-006 -1.5285e-006 v Velocity[Y] -0.20391 0.91286 0.010696 0.010696 v Velocity[Z] -5.6293e-014 6.5097e-014 -1.3477e-016 -1.3477e-016 v ǁVelocityǁ 0.00065321 0.91318 0.052286 0.052286 v Pressure -1.0013 1.0068 -3.1974e-016 2.4937e-016 v TempK 295.02 302.9 296.97 296.97 v Density 1 1 1 1 v CourantNb 0.20382 8 7.5106 7.5106 v FourierNb 0.16645 10 1.4206 1.4206 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38964 28.084 3.0792 3.0792 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 294.99 303.15 296.99 296.98 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57318 17.719 8.9312 8.9312 INSTANT 0.327000000E+02 TIME STEP NUMBER 327 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.16137E-03 0.42316E-01 Friction velocity uk : 0.16137E-03 0.42316E-01 Dimensionless distance yplus : 0.55114E-01 0.14452E+02 Friction thermal sca. tstar : -0.53917E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.39130E-01 0.10261E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74532E-04 114 0.26175E+00 0.30157E-02 0.75685E+00 c Velocity[X] 0.54219E-03 c Velocity[Y] 0.24735E-02 c Velocity[Z] 0.51199E-29 c Pressure 0.32724E-03 10 0.12595E-07 0.24698E-01 0.11593E-02 c TempK 0.27857E+02 93 0.61091E-03 0.14654E-01 0.32886E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1552 0.16207 1.2617e-005 1.2617e-005 v Velocity[Y] -0.17629 0.88083 0.010656 0.010656 v Velocity[Z] -5.3558e-014 6.5355e-014 -1.3527e-016 -1.3527e-016 v ǁVelocityǁ 0.00020189 0.88084 0.052394 0.052394 v Pressure -1.0013 1.0064 -4.4409e-017 6.9389e-016 v TempK 295.07 302.85 296.97 296.97 v Density 1 1 1 1 v CourantNb 0.35622 8 7.5479 7.5479 v FourierNb 0.17306 10 1.3842 1.3842 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36941 28.064 3.0019 3.0019 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.02 303.15 297.01 297 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.61939 17.794 8.9321 8.9321 INSTANT 0.328000000E+02 TIME STEP NUMBER 328 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.75353E-03 0.49397E-01 Friction velocity uk : 0.75353E-03 0.49397E-01 Dimensionless distance yplus : 0.25735E+00 0.16871E+02 Friction thermal sca. tstar : -0.47462E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.18272E+00 0.11978E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74871E-04 118 0.24718E+00 0.29283E-02 0.73223E+00 c Velocity[X] 0.54433E-03 c Velocity[Y] 0.23840E-02 c Velocity[Z] 0.47692E-29 c Pressure 0.33087E-03 10 0.12401E-07 0.26019E-01 0.11311E-02 c TempK 0.27805E+02 91 0.63639E-03 0.16435E-01 0.34829E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14945 0.15941 5.312e-006 5.312e-006 v Velocity[Y] -0.21785 0.90176 0.010522 0.010522 v Velocity[Z] -5.9302e-014 6.5143e-014 -1.2262e-016 -1.2262e-016 v ǁVelocityǁ 0.00030835 0.91016 0.052341 0.052341 v Pressure -1.0009 1.0066 -3.2863e-016 2.2768e-016 v TempK 295.15 302.87 296.98 296.98 v Density 1 1 1 1 v CourantNb 0.20279 8 7.5925 7.5925 v FourierNb 0.17928 10 1.3386 1.3386 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40539 28.461 2.9009 2.9009 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.07 303.15 297.01 297 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.89664 17.762 8.9311 8.9311 INSTANT 0.329000000E+02 TIME STEP NUMBER 329 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.51990E-03 0.41905E-01 Friction velocity uk : 0.51990E-03 0.41905E-01 Dimensionless distance yplus : 0.17756E+00 0.14312E+02 Friction thermal sca. tstar : -0.49052E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.12607E+00 0.10161E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75261E-04 113 0.25806E+00 0.31413E-02 0.76469E+00 c Velocity[X] 0.52841E-03 c Velocity[Y] 0.26129E-02 c Velocity[Z] 0.53731E-29 c Pressure 0.31671E-03 10 0.12452E-07 0.25968E-01 0.11040E-02 c TempK 0.27788E+02 92 0.67478E-03 0.13280E-01 0.30701E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18798 0.13095 1.8441e-005 1.8441e-005 v Velocity[Y] -0.21451 0.98358 0.010716 0.010716 v Velocity[Z] -6.0198e-014 7.1216e-014 -1.356e-016 -1.356e-016 v ǁVelocityǁ 0.00082362 0.98364 0.052869 0.052869 v Pressure -1.0002 1.0061 -2.5313e-015 -1.8865e-015 v TempK 295.22 302.94 296.99 296.99 v Density 1 1 1 1 v CourantNb 0.17439 8 7.4983 7.4983 v FourierNb 0.17438 10 1.3326 1.3326 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40521 28.461 2.8894 2.8894 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.15 303.15 297.02 297.01 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.90053 17.977 8.8308 8.8308 INSTANT 0.330000000E+02 TIME STEP NUMBER 330 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.64398E-03 0.49111E-01 Friction velocity uk : 0.64398E-03 0.49111E-01 Dimensionless distance yplus : 0.21994E+00 0.16773E+02 Friction thermal sca. tstar : -0.37604E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.15615E+00 0.11908E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.79058E-04 115 0.24409E+00 0.33842E-02 0.80611E+00 c Velocity[X] 0.56550E-03 c Velocity[Y] 0.28187E-02 c Velocity[Z] 0.48112E-29 c Pressure 0.32813E-03 10 0.12657E-07 0.30286E-01 0.10761E-02 c TempK 0.27902E+02 92 0.51449E-03 0.11937E-01 0.28477E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17676 0.18527 7.5156e-006 7.5156e-006 v Velocity[Y] -0.25852 1.0434 0.010568 0.010568 v Velocity[Z] -6.2271e-014 6.5651e-014 -1.2891e-016 -1.2891e-016 v ǁVelocityǁ 0.00023262 1.0443 0.052702 0.052702 v Pressure -0.99965 1.0063 -3.0198e-016 2.8189e-016 v TempK 295.25 302.92 297.01 297.01 v Density 1 1 1 1 v CourantNb 0.39005 8 7.5886 7.5886 v FourierNb 0.16472 10 1.2908 1.2908 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39963 24.986 2.79 2.79 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.22 303.15 297.03 297.02 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.76535 17.492 8.8794 8.8794 INSTANT 0.331000000E+02 TIME STEP NUMBER 331 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14424E-02 0.38471E-01 Friction velocity uk : 0.14424E-02 0.38471E-01 Dimensionless distance yplus : 0.49264E+00 0.13139E+02 Friction thermal sca. tstar : -0.48187E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.34976E+00 0.93286E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.81267E-04 112 0.26151E+00 0.34064E-02 0.83409E+00 c Velocity[X] 0.52756E-03 c Velocity[Y] 0.28789E-02 c Velocity[Z] 0.51026E-29 c Pressure 0.31631E-03 9 0.13680E-07 0.30520E-01 0.11279E-02 c TempK 0.27926E+02 91 0.58792E-03 0.10802E-01 0.27304E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15969 0.17093 9.9139e-006 9.9139e-006 v Velocity[Y] -0.27413 0.82889 0.010365 0.010365 v Velocity[Z] -5.9825e-014 6.2555e-014 -1.2704e-016 -1.2704e-016 v ǁVelocityǁ 0.00026305 0.8289 0.052517 0.052517 v Pressure -0.99962 1.0084 -1.2346e-015 -6.9389e-016 v TempK 295.24 302.9 297.02 297.02 v Density 1 1 1 1 v CourantNb 0.34581 8 7.5713 7.5713 v FourierNb 0.15236 10 1.2813 1.2813 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38638 26.897 2.7694 2.7694 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.25 303.15 297.05 297.04 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.77429 17.451 8.8526 8.8526 INSTANT 0.332000000E+02 TIME STEP NUMBER 332 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11227E-02 0.47633E-01 Friction velocity uk : 0.11227E-02 0.47633E-01 Dimensionless distance yplus : 0.38344E+00 0.16268E+02 Friction thermal sca. tstar : -0.32529E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.27224E+00 0.11550E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76188E-04 116 0.27500E+00 0.30339E-02 0.77444E+00 c Velocity[X] 0.48095E-03 c Velocity[Y] 0.25530E-02 c Velocity[Z] 0.48490E-29 c Pressure 0.32248E-03 9 0.14221E-07 0.30968E-01 0.11172E-02 c TempK 0.27859E+02 91 0.46907E-03 0.10526E-01 0.27973E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15903 0.18035 7.1113e-007 7.1113e-007 v Velocity[Y] -0.24452 0.9053 0.010467 0.010467 v Velocity[Z] -5.9789e-014 5.8693e-014 -1.372e-016 -1.372e-016 v ǁVelocityǁ 0.000123 0.90725 0.053009 0.053009 v Pressure -0.99957 1.0064 -2.4869e-016 3.6863e-016 v TempK 295.21 302.9 297.02 297.02 v Density 1 1 1 1 v CourantNb 0.049141 8 7.5209 7.5209 v FourierNb 0.16759 10 1.2831 1.2831 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38502 26.339 2.7744 2.7744 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.24 303.15 297.06 297.05 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.46234 17.79 8.804 8.804 INSTANT 0.333000000E+02 TIME STEP NUMBER 333 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.70725E-03 0.39534E-01 Friction velocity uk : 0.70725E-03 0.39534E-01 Dimensionless distance yplus : 0.24155E+00 0.13502E+02 Friction thermal sca. tstar : -0.59287E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.17149E+00 0.95863E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76956E-04 116 0.26196E+00 0.30405E-02 0.76138E+00 c Velocity[X] 0.52616E-03 c Velocity[Y] 0.25143E-02 c Velocity[Z] 0.43707E-29 c Pressure 0.32499E-03 10 0.13947E-07 0.32846E-01 0.10590E-02 c TempK 0.27810E+02 91 0.77563E-03 0.92674E-02 0.27615E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16386 0.1522 2.7327e-005 2.7327e-005 v Velocity[Y] -0.20876 0.96396 0.010445 0.010445 v Velocity[Z] -6.0743e-014 6.2059e-014 -1.2583e-016 -1.2583e-016 v ǁVelocityǁ 0.0002523 0.96463 0.053219 0.053219 v Pressure -0.99943 1.005 -2.7534e-016 3.1442e-016 v TempK 295.17 302.9 297.03 297.03 v Density 1 1 1 1 v CourantNb 0.60994 8 7.596 7.596 v FourierNb 0.18435 10 1.2727 1.2727 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41356 21.346 2.7507 2.7507 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.21 303.15 297.06 297.05 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0995 17.004 8.8687 8.8687 INSTANT 0.334000000E+02 TIME STEP NUMBER 334 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.58958E-03 0.43875E-01 Friction velocity uk : 0.58958E-03 0.43875E-01 Dimensionless distance yplus : 0.20136E+00 0.14985E+02 Friction thermal sca. tstar : -0.56909E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.14296E+00 0.10639E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74893E-04 117 0.25732E+00 0.30221E-02 0.75858E+00 c Velocity[X] 0.54257E-03 c Velocity[Y] 0.24796E-02 c Velocity[Z] 0.47253E-29 c Pressure 0.32734E-03 9 0.12084E-07 0.32347E-01 0.10213E-02 c TempK 0.27859E+02 90 0.52191E-03 0.98610E-02 0.30655E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18845 0.17492 -8.1896e-006 -8.1896e-006 v Velocity[Y] -0.22727 0.83456 0.010449 0.010449 v Velocity[Z] -5.926e-014 6.3262e-014 -1.2425e-016 -1.2425e-016 v ǁVelocityǁ 0.00067372 0.83946 0.053157 0.053157 v Pressure -0.99936 1.0063 -4.0856e-016 2.1684e-016 v TempK 295.16 302.89 297.03 297.03 v Density 1 1 1 1 v CourantNb 0.31851 8 7.5832 7.5832 v FourierNb 0.17348 10 1.2723 1.2723 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.44352 21.736 2.7508 2.7508 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.17 303.15 297.07 297.06 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57372 17.975 8.8555 8.8555 INSTANT 0.335000000E+02 TIME STEP NUMBER 335 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.17924E-03 0.41743E-01 Friction velocity uk : 0.17924E-03 0.41743E-01 Dimensionless distance yplus : 0.61215E-01 0.14257E+02 Friction thermal sca. tstar : -0.10750E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.43462E-01 0.10122E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75132E-04 115 0.27747E+00 0.29812E-02 0.75213E+00 c Velocity[X] 0.49239E-03 c Velocity[Y] 0.24888E-02 c Velocity[Z] 0.43599E-29 c Pressure 0.31048E-03 10 0.12778E-07 0.29446E-01 0.11535E-02 c TempK 0.27932E+02 89 0.63945E-03 0.82148E-02 0.26805E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1648 0.18825 6.3672e-006 6.3672e-006 v Velocity[Y] -0.22026 0.79318 0.010519 0.010519 v Velocity[Z] -5.664e-014 5.4788e-014 -1.2685e-016 -1.2685e-016 v ǁVelocityǁ 0.00051239 0.79621 0.053798 0.053798 v Pressure -0.99928 1.0061 2.8511e-015 3.5128e-015 v TempK 295.17 302.93 297.04 297.04 v Density 1 1 1 1 v CourantNb 0.41075 8 7.5614 7.5614 v FourierNb 0.17814 10 1.2731 1.2731 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38025 22.649 2.7529 2.7529 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.16 303.15 297.07 297.06 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.69504 17.962 8.8346 8.8346 INSTANT 0.336000000E+02 TIME STEP NUMBER 336 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.97045E-03 0.43885E-01 Friction velocity uk : 0.97045E-03 0.43885E-01 Dimensionless distance yplus : 0.33144E+00 0.14988E+02 Friction thermal sca. tstar : -0.33209E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.23532E+00 0.10641E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 336, Physical time 0.33600E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: 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 0.72267E-04 118 0.26757E+00 0.29660E-02 0.74745E+00 c Velocity[X] 0.49839E-03 c Velocity[Y] 0.24676E-02 c Velocity[Z] 0.45644E-29 c Pressure 0.32836E-03 14 0.17205E-07 0.31167E-01 0.10827E-02 c TempK 0.28058E+02 88 0.41016E-03 0.57888E-02 0.22857E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18579 0.1698 -2.6375e-006 -2.6375e-006 v Velocity[Y] -0.19756 0.90537 0.010626 0.010626 v Velocity[Z] -5.5893e-014 5.8125e-014 -1.3657e-016 -1.3657e-016 v ǁVelocityǁ 0.00039793 0.91047 0.053404 0.053404 v Pressure -0.99913 1.0069 -1.2612e-015 -6.8305e-016 v TempK 295.17 303.05 297.05 297.05 v Density 1 1 1 1 v CourantNb 0.34112 8 7.6077 7.6077 v FourierNb 0.18588 10 1.2608 1.2608 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39678 21.346 2.7278 2.7278 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.17 303.15 297.08 297.07 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.78915 17.76 8.8684 8.8684 INSTANT 0.337000000E+02 TIME STEP NUMBER 337 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12676E-03 0.46233E-01 Friction velocity uk : 0.12676E-03 0.46233E-01 Dimensionless distance yplus : 0.43294E-01 0.15790E+02 Friction thermal sca. tstar : -0.47952E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.30738E-01 0.11211E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74525E-04 111 0.25874E+00 0.30227E-02 0.74815E+00 c Velocity[X] 0.54173E-03 c Velocity[Y] 0.24810E-02 c Velocity[Z] 0.43021E-29 c Pressure 0.32446E-03 10 0.16751E-07 0.35707E-01 0.10058E-02 c TempK 0.27886E+02 88 0.46758E-03 0.66375E-02 0.23942E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16355 0.19557 1.3656e-005 1.3656e-005 v Velocity[Y] -0.24254 0.84287 0.010551 0.010551 v Velocity[Z] -4.9935e-014 5.6919e-014 -1.4896e-016 -1.4896e-016 v ǁVelocityǁ 0.00060822 0.84756 0.053624 0.053624 v Pressure -0.99912 1.0064 -1.5898e-015 -1.03e-015 v TempK 295.14 303.08 297.07 297.07 v Density 1 1 1 1 v CourantNb 0.25747 8 7.5683 7.5683 v FourierNb 0.18738 10 1.2293 1.2293 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.419 21.346 2.6544 2.6544 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.17 303.15 297.09 297.09 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.78418 17.612 8.7976 8.7976 INSTANT 0.338000000E+02 TIME STEP NUMBER 338 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.59423E-03 0.45664E-01 Friction velocity uk : 0.59423E-03 0.45664E-01 Dimensionless distance yplus : 0.20295E+00 0.15596E+02 Friction thermal sca. tstar : -0.37285E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.14409E+00 0.11073E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74738E-04 118 0.25373E+00 0.30878E-02 0.77724E+00 c Velocity[X] 0.55055E-03 c Velocity[Y] 0.25372E-02 c Velocity[Z] 0.50391E-29 c Pressure 0.31697E-03 10 0.17124E-07 0.39700E-01 0.10409E-02 c TempK 0.27847E+02 86 0.42926E-03 0.47790E-02 0.21643E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17241 0.18306 -1.1308e-005 -1.1308e-005 v Velocity[Y] -0.17732 0.86445 0.010329 0.010329 v Velocity[Z] -4.4955e-014 6.386e-014 -1.2898e-016 -1.2898e-016 v ǁVelocityǁ 0.00061451 0.86668 0.052922 0.052922 v Pressure -0.99916 1.008 -8.1712e-016 -2.6021e-016 v TempK 295.1 303.18 297.08 297.08 v Density 1 1 1 1 v CourantNb 0.18485 8 7.6068 7.6068 v FourierNb 0.17932 10 1.2156 1.2156 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41355 21.346 2.6255 2.6255 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.14 303.15 297.11 297.1 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.97105 17.87 8.8224 8.8224 INSTANT 0.339000000E+02 TIME STEP NUMBER 339 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11684E-02 0.49840E-01 Friction velocity uk : 0.11684E-02 0.49840E-01 Dimensionless distance yplus : 0.39903E+00 0.17022E+02 Friction thermal sca. tstar : -0.64354E+01 0.75904E-01 Rough dim-less th. sca. tplus : 0.28330E+00 0.12085E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73151E-04 113 0.27366E+00 0.30880E-02 0.76570E+00 c Velocity[X] 0.49572E-03 c Velocity[Y] 0.25923E-02 c Velocity[Z] 0.48453E-29 c Pressure 0.30164E-03 9 0.15843E-07 0.36609E-01 0.88913E-03 c TempK 0.27660E+02 87 0.40669E-03 0.39285E-02 0.19177E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18131 0.16931 6.6831e-006 6.6831e-006 v Velocity[Y] -0.18206 0.80402 0.010421 0.010421 v Velocity[Z] -5.8914e-014 6.9402e-014 -1.2331e-016 -1.2331e-016 v ǁVelocityǁ 0.00016775 0.80441 0.053087 0.053087 v Pressure -0.99934 1.0052 -4.2633e-016 1.9516e-016 v TempK 295.06 303.22 297.09 297.09 v Density 1 1 1 1 v CourantNb 0.27869 8 7.5428 7.5428 v FourierNb 0.18254 10 1.2227 1.2227 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40509 21.346 2.6415 2.6415 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.1 303.18 297.12 297.11 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.61143 17.41 8.7655 8.7655 INSTANT 0.340000000E+02 TIME STEP NUMBER 340 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.18047E-03 0.44749E-01 Friction velocity uk : 0.18047E-03 0.44749E-01 Dimensionless distance yplus : 0.61635E-01 0.15283E+02 Friction thermal sca. tstar : -0.14917E+02 0.10273E+00 Rough dim-less th. sca. tplus : 0.43760E-01 0.10851E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71143E-04 114 0.25007E+00 0.30460E-02 0.75249E+00 c Velocity[X] 0.50176E-03 c Velocity[Y] 0.25442E-02 c Velocity[Z] 0.48723E-29 c Pressure 0.30314E-03 10 0.14252E-07 0.36363E-01 0.94660E-03 c TempK 0.27602E+02 84 0.44952E-03 0.28795E-02 0.17264E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14967 0.16222 1.038e-005 1.038e-005 v Velocity[Y] -0.17237 0.90611 0.010573 0.010573 v Velocity[Z] -6.2982e-014 6.2611e-014 -1.195e-016 -1.195e-016 v ǁVelocityǁ 0.00068533 0.90938 0.052981 0.052981 v Pressure -0.99948 1.0075 -5.1514e-016 1.5179e-016 v TempK 295.05 303.24 297.1 297.1 v Density 1 1 1 1 v CourantNb 0.053506 8 7.5421 7.5421 v FourierNb 0.17156 10 1.2293 1.2293 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3662 21.346 2.6563 2.6563 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.06 303.22 297.13 297.12 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.83436 17.755 8.7714 8.7714 INSTANT 0.341000000E+02 TIME STEP NUMBER 341 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10961E-02 0.46116E-01 Friction velocity uk : 0.10961E-02 0.46116E-01 Dimensionless distance yplus : 0.37434E+00 0.15750E+02 Friction thermal sca. tstar : -0.33658E+01 0.15274E+00 Rough dim-less th. sca. tplus : 0.26578E+00 0.11182E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72897E-04 117 0.25802E+00 0.31854E-02 0.77867E+00 c Velocity[X] 0.52132E-03 c Velocity[Y] 0.26641E-02 c Velocity[Z] 0.45552E-29 c Pressure 0.30778E-03 10 0.13127E-07 0.36219E-01 0.99820E-03 c TempK 0.27574E+02 83 0.37487E-03 0.30942E-02 0.17244E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15223 0.11758 2.0838e-005 2.0838e-005 v Velocity[Y] -0.17928 0.89277 0.01043 0.01043 v Velocity[Z] -6.156e-014 6.3113e-014 -1.3308e-016 -1.3308e-016 v ǁVelocityǁ 0.00087932 0.89679 0.052909 0.052909 v Pressure -0.99959 1.0067 1.4211e-016 6.8305e-016 v TempK 295.08 303.3 297.11 297.11 v Density 1 1 1 1 v CourantNb 0.13236 8 7.5291 7.5291 v FourierNb 0.17338 10 1.2394 1.2394 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39793 21.346 2.6787 2.6787 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.05 303.24 297.14 297.13 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75185 17.911 8.7685 8.7685 INSTANT 0.342000000E+02 TIME STEP NUMBER 342 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11722E-02 0.43647E-01 Friction velocity uk : 0.11722E-02 0.43647E-01 Dimensionless distance yplus : 0.40036E+00 0.14907E+02 Friction thermal sca. tstar : -0.27677E+01 0.33237E+00 Rough dim-less th. sca. tplus : 0.28425E+00 0.10584E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70311E-04 114 0.26190E+00 0.29398E-02 0.74424E+00 c Velocity[X] 0.49645E-03 c Velocity[Y] 0.24433E-02 c Velocity[Z] 0.44061E-29 c Pressure 0.31025E-03 10 0.14422E-07 0.35493E-01 0.97379E-03 c TempK 0.27444E+02 84 0.32214E-03 0.26695E-02 0.15794E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20244 0.18136 5.4827e-006 5.4827e-006 v Velocity[Y] -0.19943 0.79467 0.010398 0.010398 v Velocity[Z] -6.176e-014 5.9495e-014 -1.2157e-016 -1.2157e-016 v ǁVelocityǁ 0.00036356 0.7981 0.052629 0.052629 v Pressure -0.99955 1.0069 -9.6811e-016 -4.0115e-016 v TempK 295.12 303.31 297.12 297.12 v Density 1 1 1 1 v CourantNb 0.46256 8 7.5414 7.5414 v FourierNb 0.18604 10 1.2463 1.2463 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39712 21.346 2.6951 2.6951 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.08 303.3 297.15 297.14 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.84554 17.58 8.7877 8.7877 INSTANT 0.343000000E+02 TIME STEP NUMBER 343 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.61146E-03 0.43399E-01 Friction velocity uk : 0.61146E-03 0.43399E-01 Dimensionless distance yplus : 0.20883E+00 0.14822E+02 Friction thermal sca. tstar : -0.32420E+01 0.31704E+00 Rough dim-less th. sca. tplus : 0.14827E+00 0.10523E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69721E-04 114 0.24405E+00 0.30122E-02 0.74833E+00 c Velocity[X] 0.53594E-03 c Velocity[Y] 0.24762E-02 c Velocity[Z] 0.42992E-29 c Pressure 0.31378E-03 10 0.13213E-07 0.34272E-01 0.10012E-02 c TempK 0.27324E+02 83 0.43678E-03 0.28266E-02 0.16443E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15538 0.16546 2.5725e-005 2.5725e-005 v Velocity[Y] -0.22015 0.92782 0.010497 0.010497 v Velocity[Z] -6.013e-014 5.5789e-014 -1.4412e-016 -1.4412e-016 v ǁVelocityǁ 0.00011786 0.92813 0.053265 0.053265 v Pressure -0.99961 1.0076 -1.0658e-016 4.6621e-016 v TempK 295.15 303.38 297.13 297.13 v Density 1 1 1 1 v CourantNb 0.24304 8 7.5392 7.5392 v FourierNb 0.1686 10 1.2553 1.2553 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39774 21.346 2.7162 2.7162 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.12 303.31 297.16 297.15 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.63676 17.684 8.7946 8.7946 INSTANT 0.344000000E+02 TIME STEP NUMBER 344 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.44738E-03 0.42023E-01 Friction velocity uk : 0.44738E-03 0.42023E-01 Dimensionless distance yplus : 0.15279E+00 0.14352E+02 Friction thermal sca. tstar : -0.79643E+01 0.47836E+00 Rough dim-less th. sca. tplus : 0.10848E+00 0.10190E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73808E-04 118 0.26571E+00 0.32968E-02 0.80303E+00 c Velocity[X] 0.53040E-03 c Velocity[Y] 0.27664E-02 c Velocity[Z] 0.42803E-29 c Pressure 0.29042E-03 9 0.15775E-07 0.30926E-01 0.98678E-03 c TempK 0.27390E+02 83 0.32825E-03 0.29783E-02 0.17716E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15509 0.16454 1.8291e-006 1.8291e-006 v Velocity[Y] -0.23741 0.823 0.010268 0.010268 v Velocity[Z] -5.0924e-014 5.5577e-014 -1.1604e-016 -1.1604e-016 v ǁVelocityǁ 5.8232e-005 0.82827 0.052427 0.052427 v Pressure -0.99968 1.0076 -4.0856e-016 1.7347e-016 v TempK 295.15 303.39 297.14 297.14 v Density 1 1 1 1 v CourantNb 0.15361 8 7.5908 7.5908 v FourierNb 0.18351 10 1.2611 1.2611 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40056 21.968 2.7291 2.7291 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.15 303.38 297.17 297.16 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.84952 17.852 8.8519 8.8519 INSTANT 0.345000000E+02 TIME STEP NUMBER 345 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.41292E-03 0.43227E-01 Friction velocity uk : 0.41292E-03 0.43227E-01 Dimensionless distance yplus : 0.14102E+00 0.14763E+02 Friction thermal sca. tstar : -0.71306E+01 0.40849E+00 Rough dim-less th. sca. tplus : 0.10012E+00 0.10482E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71926E-04 116 0.25557E+00 0.31705E-02 0.78320E+00 c Velocity[X] 0.46417E-03 c Velocity[Y] 0.27063E-02 c Velocity[Z] 0.43423E-29 c Pressure 0.30465E-03 10 0.12271E-07 0.31329E-01 0.10159E-02 c TempK 0.27345E+02 83 0.49099E-03 0.35267E-02 0.17554E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14821 0.17323 2.4411e-005 2.4411e-005 v Velocity[Y] -0.2461 0.80648 0.010491 0.010491 v Velocity[Z] -5.9575e-014 5.8731e-014 -1.3369e-016 -1.3369e-016 v ǁVelocityǁ 0.00032271 0.80663 0.052765 0.052765 v Pressure -0.99963 1.0082 -1.1546e-015 -5.7463e-016 v TempK 295.13 303.41 297.15 297.15 v Density 1 1 1 1 v CourantNb 0.079998 8 7.5426 7.5426 v FourierNb 0.16954 10 1.273 1.273 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37782 24.165 2.7562 2.7562 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.15 303.39 297.18 297.17 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.50893 17.882 8.8156 8.8156 INSTANT 0.346000000E+02 TIME STEP NUMBER 346 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.62769E-03 0.46718E-01 Friction velocity uk : 0.62769E-03 0.46718E-01 Dimensionless distance yplus : 0.21438E+00 0.15956E+02 Friction thermal sca. tstar : -0.42584E+01 0.51354E+00 Rough dim-less th. sca. tplus : 0.15220E+00 0.11328E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70461E-04 112 0.25217E+00 0.32241E-02 0.78958E+00 c Velocity[X] 0.51633E-03 c Velocity[Y] 0.27077E-02 c Velocity[Z] 0.41525E-29 c Pressure 0.30762E-03 9 0.11324E-07 0.30761E-01 0.91241E-03 c TempK 0.27365E+02 84 0.33760E-03 0.22178E-02 0.14488E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17964 0.17653 -1.1011e-005 -1.1011e-005 v Velocity[Y] -0.24195 0.83694 0.010431 0.010431 v Velocity[Z] -5.2665e-014 6.0747e-014 -1.2381e-016 -1.2381e-016 v ǁVelocityǁ 0.0002581 0.83705 0.052453 0.052453 v Pressure -0.99956 1.0054 -3.1974e-016 2.2768e-016 v TempK 295.13 303.41 297.17 297.17 v Density 1 1 1 1 v CourantNb 0.15856 8 7.545 7.545 v FourierNb 0.16152 10 1.2822 1.2822 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34477 22.895 2.7772 2.7772 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.13 303.41 297.19 297.18 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.36021 17.74 8.8272 8.8272 INSTANT 0.347000000E+02 TIME STEP NUMBER 347 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.50218E-03 0.45849E-01 Friction velocity uk : 0.50218E-03 0.45849E-01 Dimensionless distance yplus : 0.17151E+00 0.15659E+02 Friction thermal sca. tstar : -0.51654E+01 0.49357E+00 Rough dim-less th. sca. tplus : 0.12177E+00 0.11118E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73094E-04 112 0.27346E+00 0.33054E-02 0.81337E+00 c Velocity[X] 0.53998E-03 c Velocity[Y] 0.27654E-02 c Velocity[Z] 0.42718E-29 c Pressure 0.30125E-03 10 0.13020E-07 0.29391E-01 0.90449E-03 c TempK 0.27292E+02 85 0.42628E-03 0.26955E-02 0.15218E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17047 0.18333 3.5618e-006 3.5618e-006 v Velocity[Y] -0.24736 0.85014 0.010287 0.010287 v Velocity[Z] -4.8341e-014 5.656e-014 -1.5624e-016 -1.5624e-016 v ǁVelocityǁ 0.00013313 0.85016 0.052331 0.052331 v Pressure -0.99968 1.0075 -6.1284e-016 -3.2526e-017 v TempK 295.16 303.26 297.18 297.18 v Density 1 1 1 1 v CourantNb 0.46973 8 7.5487 7.5487 v FourierNb 0.17767 10 1.2913 1.2913 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37925 25.184 2.7978 2.7978 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.13 303.41 297.21 297.2 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.83248 17.559 8.84 8.84 INSTANT 0.348000000E+02 TIME STEP NUMBER 348 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.58452E-03 0.45552E-01 Friction velocity uk : 0.58452E-03 0.45552E-01 Dimensionless distance yplus : 0.19963E+00 0.15558E+02 Friction thermal sca. tstar : -0.66718E+01 0.28410E+00 Rough dim-less th. sca. tplus : 0.14174E+00 0.11046E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70659E-04 114 0.26821E+00 0.31579E-02 0.79268E+00 c Velocity[X] 0.49049E-03 c Velocity[Y] 0.26674E-02 c Velocity[Z] 0.44566E-29 c Pressure 0.29374E-03 10 0.17242E-07 0.27993E-01 0.10060E-02 c TempK 0.27165E+02 85 0.37068E-03 0.33212E-02 0.16947E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15242 0.17214 -6.7803e-006 -6.7803e-006 v Velocity[Y] -0.22477 0.81293 0.010394 0.010394 v Velocity[Z] -5.0709e-014 5.4727e-014 -1.2222e-016 -1.2222e-016 v ǁVelocityǁ 0.00043857 0.82159 0.05248 0.05248 v Pressure -1 1.005 2.931e-016 8.782e-016 v TempK 295.2 303.3 297.18 297.18 v Density 1 1 1 1 v CourantNb 0.55931 8 7.5292 7.5292 v FourierNb 0.18768 10 1.303 1.303 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40061 27.703 2.8249 2.8249 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.16 303.26 297.22 297.21 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81697 17.981 8.8322 8.8322 INSTANT 0.349000000E+02 TIME STEP NUMBER 349 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.23059E-03 0.43920E-01 Friction velocity uk : 0.23059E-03 0.43920E-01 Dimensionless distance yplus : 0.78754E-01 0.15000E+02 Friction thermal sca. tstar : -0.42829E+01 0.20322E+00 Rough dim-less th. sca. tplus : 0.55914E-01 0.10650E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71212E-04 111 0.25735E+00 0.30549E-02 0.75888E+00 c Velocity[X] 0.50892E-03 c Velocity[Y] 0.25460E-02 c Velocity[Z] 0.47158E-29 c Pressure 0.30851E-03 10 0.10691E-07 0.28121E-01 0.86271E-03 c TempK 0.27035E+02 85 0.51818E-03 0.24457E-02 0.15400E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16275 0.16871 1.1929e-006 1.1929e-006 v Velocity[Y] -0.21847 0.8086 0.010562 0.010562 v Velocity[Z] -5.7835e-014 5.3406e-014 -1.4727e-016 -1.4727e-016 v ǁVelocityǁ 0.00021594 0.80874 0.052399 0.052399 v Pressure -1.0002 1.007 -9.9476e-016 -4.0115e-016 v TempK 295.22 303.33 297.19 297.19 v Density 1 1 1 1 v CourantNb 0.28582 8 7.5802 7.5802 v FourierNb 0.17994 10 1.2953 1.2953 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40084 25.152 2.8069 2.8069 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.2 303.3 297.22 297.21 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81478 17.726 8.8755 8.8755 INSTANT 0.350000000E+02 TIME STEP NUMBER 350 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.33822E-03 0.44000E-01 Friction velocity uk : 0.33822E-03 0.44000E-01 Dimensionless distance yplus : 0.11551E+00 0.15027E+02 Friction thermal sca. tstar : -0.31535E+01 0.21201E+00 Rough dim-less th. sca. tplus : 0.82012E-01 0.10669E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71484E-04 116 0.26635E+00 0.32228E-02 0.80164E+00 c Velocity[X] 0.55107E-03 c Velocity[Y] 0.26717E-02 c Velocity[Z] 0.45185E-29 c Pressure 0.31323E-03 10 0.12164E-07 0.27625E-01 0.98739E-03 c TempK 0.27008E+02 85 0.33039E-03 0.24811E-02 0.16221E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20533 0.16561 -1.4347e-005 -1.4347e-005 v Velocity[Y] -0.23551 0.89763 0.010367 0.010367 v Velocity[Z] -6.0102e-014 5.1188e-014 -1.2496e-016 -1.2496e-016 v ǁVelocityǁ 0.00012579 0.89829 0.052125 0.052125 v Pressure -1.0005 1.0075 -1.35e-015 -7.9147e-016 v TempK 295.23 303.27 297.21 297.21 v Density 1 1 1 1 v CourantNb 0.16102 8 7.5441 7.5441 v FourierNb 0.17443 10 1.3114 1.3114 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41766 27.667 2.8432 2.8432 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.22 303.33 297.23 297.22 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.59009 17.604 8.8555 8.8555 INSTANT 0.351000000E+02 TIME STEP NUMBER 351 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32392E-03 0.41673E-01 Friction velocity uk : 0.32392E-03 0.41673E-01 Dimensionless distance yplus : 0.11063E+00 0.14232E+02 Friction thermal sca. tstar : -0.65006E+01 0.23733E+00 Rough dim-less th. sca. tplus : 0.78544E-01 0.10105E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71252E-04 111 0.26595E+00 0.31333E-02 0.80061E+00 c Velocity[X] 0.53840E-03 c Velocity[Y] 0.25949E-02 c Velocity[Z] 0.43836E-29 c Pressure 0.30210E-03 10 0.11978E-07 0.25578E-01 0.98583E-03 c TempK 0.26876E+02 84 0.44757E-03 0.22573E-02 0.15188E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1926 0.17498 -7.8131e-006 -7.8131e-006 v Velocity[Y] -0.22199 0.75119 0.010285 0.010285 v Velocity[Z] -5.9617e-014 5.1634e-014 -1.3411e-016 -1.3411e-016 v ǁVelocityǁ 0.00032869 0.75215 0.05231 0.05231 v Pressure -1.0005 1.0061 8.8818e-017 6.3968e-016 v TempK 295.22 303.26 297.22 297.22 v Density 1 1 1 1 v CourantNb 0.36914 8 7.5399 7.5399 v FourierNb 0.18107 10 1.3281 1.3281 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.43069 28.461 2.881 2.881 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.23 303.27 297.24 297.24 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.64651 17.999 8.868 8.868 INSTANT 0.352000000E+02 TIME STEP NUMBER 352 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.69700E-03 0.43991E-01 Friction velocity uk : 0.69700E-03 0.43991E-01 Dimensionless distance yplus : 0.23805E+00 0.15024E+02 Friction thermal sca. tstar : -0.97968E+01 0.26048E+00 Rough dim-less th. sca. tplus : 0.16901E+00 0.10667E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70427E-04 115 0.25751E+00 0.30736E-02 0.78299E+00 c Velocity[X] 0.50544E-03 c Velocity[Y] 0.25682E-02 c Velocity[Z] 0.46427E-29 c Pressure 0.29299E-03 9 0.11999E-07 0.23590E-01 0.96678E-03 c TempK 0.26881E+02 85 0.36813E-03 0.24231E-02 0.14695E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18208 0.16344 -1.1845e-005 -1.1845e-005 v Velocity[Y] -0.21723 0.80115 0.010357 0.010357 v Velocity[Z] -5.4078e-014 5.2124e-014 -1.2011e-016 -1.2011e-016 v ǁVelocityǁ 0.00034819 0.80132 0.052406 0.052406 v Pressure -1.0001 1.0073 -3.6415e-016 2.7105e-016 v TempK 295.2 303.25 297.23 297.23 v Density 1 1 1 1 v CourantNb 0.17986 8 7.5902 7.5902 v FourierNb 0.17031 10 1.3286 1.3286 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.42953 28.461 2.8834 2.8834 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.22 303.26 297.26 297.25 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.61478 17.541 8.9188 8.9188 INSTANT 0.353000000E+02 TIME STEP NUMBER 353 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.30980E-03 0.42273E-01 Friction velocity uk : 0.30980E-03 0.42273E-01 Dimensionless distance yplus : 0.10580E+00 0.14438E+02 Friction thermal sca. tstar : -0.10028E+02 0.25001E+00 Rough dim-less th. sca. tplus : 0.75120E-01 0.10250E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70860E-04 112 0.25307E+00 0.30674E-02 0.76972E+00 c Velocity[X] 0.52399E-03 c Velocity[Y] 0.25435E-02 c Velocity[Z] 0.43587E-29 c Pressure 0.30467E-03 9 0.12522E-07 0.23722E-01 0.98240E-03 c TempK 0.26969E+02 85 0.41584E-03 0.23163E-02 0.15343E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20335 0.16156 -5.7854e-006 -5.7854e-006 v Velocity[Y] -0.21294 0.84099 0.010465 0.010465 v Velocity[Z] -5.3469e-014 5.2132e-014 -1.5304e-016 -1.5304e-016 v ǁVelocityǁ 0.00018473 0.85266 0.052317 0.052317 v Pressure -0.99958 1.007 -8.0824e-016 -2.06e-016 v TempK 295.2 303.29 297.24 297.24 v Density 1 1 1 1 v CourantNb 0.30993 8 7.5939 7.5939 v FourierNb 0.18356 10 1.3198 1.3198 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40767 28.461 2.8671 2.8671 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.2 303.25 297.27 297.26 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.86479 17.809 8.9137 8.9137 INSTANT 0.354000000E+02 TIME STEP NUMBER 354 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.37747E-03 0.42653E-01 Friction velocity uk : 0.37747E-03 0.42653E-01 Dimensionless distance yplus : 0.12892E+00 0.14567E+02 Friction thermal sca. tstar : -0.55607E+01 0.25223E+00 Rough dim-less th. sca. tplus : 0.91530E-01 0.10343E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71150E-04 113 0.26242E+00 0.31275E-02 0.78469E+00 c Velocity[X] 0.54481E-03 c Velocity[Y] 0.25827E-02 c Velocity[Z] 0.42993E-29 c Pressure 0.31456E-03 9 0.12489E-07 0.25046E-01 0.11187E-02 c TempK 0.26954E+02 83 0.33524E-03 0.17238E-02 0.13615E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17657 0.15517 2.558e-007 2.558e-007 v Velocity[Y] -0.2113 0.78494 0.010458 0.010458 v Velocity[Z] -5.6106e-014 5.0187e-014 -1.369e-016 -1.369e-016 v ǁVelocityǁ 0.00039589 0.78822 0.052373 0.052373 v Pressure -0.99931 1.0067 -5.6843e-016 6.5052e-017 v TempK 295.24 303.27 297.25 297.25 v Density 1 1 1 1 v CourantNb 0.37999 8 7.5684 7.5684 v FourierNb 0.17906 10 1.3105 1.3105 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.43306 28.461 2.8465 2.8465 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.2 303.29 297.28 297.27 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.86048 17.884 8.8788 8.8788 INSTANT 0.355000000E+02 TIME STEP NUMBER 355 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28858E-03 0.43059E-01 Friction velocity uk : 0.28858E-03 0.43059E-01 Dimensionless distance yplus : 0.98559E-01 0.14706E+02 Friction thermal sca. tstar : -0.53633E+01 0.26335E+00 Rough dim-less th. sca. tplus : 0.69975E-01 0.10441E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69047E-04 109 0.26039E+00 0.30753E-02 0.77232E+00 c Velocity[X] 0.54269E-03 c Velocity[Y] 0.25326E-02 c Velocity[Z] 0.41865E-29 c Pressure 0.31174E-03 10 0.98170E-08 0.25444E-01 0.10734E-02 c TempK 0.26953E+02 83 0.46026E-03 0.21545E-02 0.15086E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16303 0.17135 -4.1993e-006 -4.1993e-006 v Velocity[Y] -0.27494 0.86716 0.010517 0.010517 v Velocity[Z] -5.2068e-014 4.9752e-014 -1.4e-016 -1.4e-016 v ǁVelocityǁ 0.00060324 0.87204 0.052306 0.052306 v Pressure -0.99949 1.0069 -7.7272e-016 -2.6021e-016 v TempK 295.29 303.27 297.26 297.26 v Density 1 1 1 1 v CourantNb 0.22802 8 7.5504 7.5504 v FourierNb 0.19401 10 1.3125 1.3125 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41415 28.461 2.8534 2.8534 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.24 303.27 297.29 297.28 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.6805 17.999 8.863 8.863 INSTANT 0.356000000E+02 TIME STEP NUMBER 356 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.13924E-03 0.43355E-01 Friction velocity uk : 0.13924E-03 0.43355E-01 Dimensionless distance yplus : 0.47556E-01 0.14807E+02 Friction thermal sca. tstar : -0.45859E+01 0.31826E+00 Rough dim-less th. sca. tplus : 0.33764E-01 0.10513E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73337E-04 109 0.27060E+00 0.31066E-02 0.78465E+00 c Velocity[X] 0.53842E-03 c Velocity[Y] 0.25682E-02 c Velocity[Z] 0.47094E-29 c Pressure 0.31092E-03 9 0.12166E-07 0.25868E-01 0.98682E-03 c TempK 0.26981E+02 83 0.33576E-03 0.19826E-02 0.13708E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16305 0.14079 -2.6062e-005 -2.6062e-005 v Velocity[Y] -0.1926 0.7869 0.010392 0.010392 v Velocity[Z] -5.7862e-014 4.9716e-014 -1.2914e-016 -1.2914e-016 v ǁVelocityǁ 0.00040764 0.7869 0.052322 0.052322 v Pressure -0.99966 1.0061 1.5277e-015 2.2009e-015 v TempK 295.35 303.32 297.27 297.27 v Density 1 1 1 1 v CourantNb 0.38695 8 7.5325 7.5325 v FourierNb 0.18646 10 1.3097 1.3097 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40079 28.461 2.8474 2.8474 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.29 303.27 297.3 297.29 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75946 17.68 8.8421 8.8421 INSTANT 0.357000000E+02 TIME STEP NUMBER 357 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.15066E-03 0.37232E-01 Friction velocity uk : 0.15066E-03 0.37232E-01 Dimensionless distance yplus : 0.51455E-01 0.12716E+02 Friction thermal sca. tstar : -0.59221E+01 0.32875E+00 Rough dim-less th. sca. tplus : 0.36532E-01 0.90281E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69654E-04 114 0.24758E+00 0.32269E-02 0.78616E+00 c Velocity[X] 0.53663E-03 c Velocity[Y] 0.26902E-02 c Velocity[Z] 0.42842E-29 c Pressure 0.31127E-03 10 0.12169E-07 0.25373E-01 0.98468E-03 c TempK 0.26944E+02 83 0.40226E-03 0.26174E-02 0.14207E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15836 0.18822 2.9752e-006 2.9752e-006 v Velocity[Y] -0.22365 0.89334 0.010514 0.010514 v Velocity[Z] -6.2408e-014 5.1734e-014 -1.2656e-016 -1.2656e-016 v ǁVelocityǁ 0.00022146 0.89334 0.052557 0.052557 v Pressure -0.99972 1.0066 -7.816e-016 -1.4095e-016 v TempK 295.38 303.37 297.27 297.27 v Density 1 1 1 1 v CourantNb 0.15105 8 7.5193 7.5193 v FourierNb 0.18176 10 1.3134 1.3134 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38798 28.461 2.8527 2.8527 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.35 303.32 297.31 297.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.44992 17.856 8.8327 8.8327 INSTANT 0.358000000E+02 TIME STEP NUMBER 358 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.52139E-03 0.40266E-01 Friction velocity uk : 0.52139E-03 0.40266E-01 Dimensionless distance yplus : 0.17807E+00 0.13752E+02 Friction thermal sca. tstar : -0.47584E+01 0.32009E+00 Rough dim-less th. sca. tplus : 0.12643E+00 0.97638E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76338E-04 112 0.27845E+00 0.34351E-02 0.83365E+00 c Velocity[X] 0.56992E-03 c Velocity[Y] 0.28652E-02 c Velocity[Z] 0.47507E-29 c Pressure 0.30240E-03 10 0.94780E-08 0.25196E-01 0.10635E-02 c TempK 0.27138E+02 83 0.33443E-03 0.28999E-02 0.15027E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21621 0.17975 -1.0434e-005 -1.0434e-005 v Velocity[Y] -0.21279 0.78408 0.010259 0.010259 v Velocity[Z] -6.3695e-014 5.4747e-014 -9.9915e-017 -9.9915e-017 v ǁVelocityǁ 9.5604e-005 0.78423 0.052501 0.052501 v Pressure -0.99976 1.0071 -3.0198e-016 3.4694e-016 v TempK 295.4 303.37 297.28 297.28 v Density 1 1 1 1 v CourantNb 0.25636 8 7.5606 7.5606 v FourierNb 0.16024 10 1.3049 1.3049 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34203 28.461 2.8262 2.8262 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.38 303.37 297.31 297.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.93205 17.844 8.8654 8.8654 INSTANT 0.359000000E+02 TIME STEP NUMBER 359 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.55136E-03 0.38970E-01 Friction velocity uk : 0.55136E-03 0.38970E-01 Dimensionless distance yplus : 0.18831E+00 0.13309E+02 Friction thermal sca. tstar : -0.11034E+02 0.31618E+00 Rough dim-less th. sca. tplus : 0.13369E+00 0.94494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69740E-04 111 0.25870E+00 0.31301E-02 0.79461E+00 c Velocity[X] 0.52990E-03 c Velocity[Y] 0.26002E-02 c Velocity[Z] 0.48640E-29 c Pressure 0.30259E-03 10 0.10743E-07 0.24725E-01 0.11533E-02 c TempK 0.27255E+02 83 0.43571E-03 0.27433E-02 0.14830E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1751 0.21652 6.7454e-006 6.7454e-006 v Velocity[Y] -0.20816 0.82758 0.010339 0.010339 v Velocity[Z] -6.3993e-014 5.2527e-014 -1.3391e-016 -1.3391e-016 v ǁVelocityǁ 0.00065847 0.82939 0.05215 0.05215 v Pressure -0.99973 1.006 -8.0824e-016 -1.1926e-016 v TempK 295.42 303.4 297.29 297.29 v Density 1 1 1 1 v CourantNb 0.2785 8 7.5024 7.5024 v FourierNb 0.17626 10 1.3117 1.3117 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37624 28.461 2.8414 2.8414 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.4 303.37 297.32 297.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.61055 17.872 8.8142 8.8142 INSTANT 0.360000000E+02 TIME STEP NUMBER 360 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.60389E-03 0.39248E-01 Friction velocity uk : 0.60389E-03 0.39248E-01 Dimensionless distance yplus : 0.20625E+00 0.13404E+02 Friction thermal sca. tstar : -0.20854E+02 0.28695E+00 Rough dim-less th. sca. tplus : 0.14643E+00 0.95168E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73035E-04 112 0.26202E+00 0.28800E-02 0.73528E+00 c Velocity[X] 0.53354E-03 c Velocity[Y] 0.23465E-02 c Velocity[Z] 0.47158E-29 c Pressure 0.32384E-03 10 0.11039E-07 0.27081E-01 0.10470E-02 c TempK 0.27177E+02 84 0.31779E-03 0.34202E-02 0.15936E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16662 0.1922 -1.3828e-005 -1.3828e-005 v Velocity[Y] -0.18798 0.81598 0.010402 0.010402 v Velocity[Z] -6.7225e-014 5.0846e-014 -1.2892e-016 -1.2892e-016 v ǁVelocityǁ 8.6565e-005 0.82345 0.05235 0.05235 v Pressure -0.99971 1.0066 -3.7303e-016 2.7105e-016 v TempK 295.45 303.34 297.3 297.3 v Density 1 1 1 1 v CourantNb 0.60017 8 7.4706 7.4706 v FourierNb 0.17574 10 1.3169 1.3169 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41359 22.397 2.8497 2.8497 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.42 303.4 297.32 297.32 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.97683 17.478 8.7876 8.7876 INSTANT 0.361000000E+02 TIME STEP NUMBER 361 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.46578E-03 0.37478E-01 Friction velocity uk : 0.46578E-03 0.37478E-01 Dimensionless distance yplus : 0.15908E+00 0.12800E+02 Friction thermal sca. tstar : -0.82999E+01 0.30589E+00 Rough dim-less th. sca. tplus : 0.11294E+00 0.90878E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69525E-04 114 0.24873E+00 0.28806E-02 0.72443E+00 c Velocity[X] 0.53185E-03 c Velocity[Y] 0.23488E-02 c Velocity[Z] 0.51278E-29 c Pressure 0.32225E-03 10 0.12050E-07 0.25566E-01 0.10895E-02 c TempK 0.27125E+02 84 0.43076E-03 0.22924E-02 0.13534E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15888 0.22505 1.0399e-005 1.0399e-005 v Velocity[Y] -0.18074 0.99276 0.010555 0.010555 v Velocity[Z] -6.0945e-014 5.0533e-014 -1.4874e-016 -1.4874e-016 v ǁVelocityǁ 0.000235 0.99424 0.052274 0.052274 v Pressure -0.99962 1.0064 2.2204e-016 7.9147e-016 v TempK 295.51 303.28 297.31 297.31 v Density 1 1 1 1 v CourantNb 0.26953 8 7.448 7.448 v FourierNb 0.18622 10 1.3255 1.3255 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39846 24.637 2.87 2.87 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.45 303.34 297.34 297.33 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.8821 17.907 8.7735 8.7735 INSTANT 0.362000000E+02 TIME STEP NUMBER 362 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10783E-02 0.42058E-01 Friction velocity uk : 0.10783E-02 0.42058E-01 Dimensionless distance yplus : 0.36827E+00 0.14364E+02 Friction thermal sca. tstar : -0.60747E+01 0.32808E+00 Rough dim-less th. sca. tplus : 0.26147E+00 0.10198E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70836E-04 114 0.26183E+00 0.30929E-02 0.74834E+00 c Velocity[X] 0.53789E-03 c Velocity[Y] 0.25551E-02 c Velocity[Z] 0.41786E-29 c Pressure 0.32659E-03 10 0.12660E-07 0.26357E-01 0.12559E-02 c TempK 0.27076E+02 86 0.31938E-03 0.29228E-02 0.15957E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16503 0.16474 -1.6068e-005 -1.6068e-005 v Velocity[Y] -0.18864 0.8673 0.01068 0.01068 v Velocity[Z] -6.3123e-014 5.1731e-014 -1.3766e-016 -1.3766e-016 v ǁVelocityǁ 0.00046695 0.87523 0.052843 0.052843 v Pressure -0.99962 1.009 -1.0036e-015 -3.2526e-016 v TempK 295.57 303.24 297.32 297.32 v Density 1 1 1 1 v CourantNb 0.36245 8 7.4762 7.4762 v FourierNb 0.17057 10 1.3194 1.3194 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38954 23.181 2.8554 2.8554 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.51 303.28 297.35 297.34 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.78992 17.969 8.7956 8.7956 INSTANT 0.363000000E+02 TIME STEP NUMBER 363 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.83993E-03 0.43250E-01 Friction velocity uk : 0.83993E-03 0.43250E-01 Dimensionless distance yplus : 0.28686E+00 0.14771E+02 Friction thermal sca. tstar : -0.37116E+01 0.38688E+00 Rough dim-less th. sca. tplus : 0.20367E+00 0.10487E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71441E-04 112 0.26650E+00 0.32066E-02 0.76074E+00 c Velocity[X] 0.57443E-03 c Velocity[Y] 0.26322E-02 c Velocity[Z] 0.51579E-29 c Pressure 0.31768E-03 9 0.14121E-07 0.26404E-01 0.11654E-02 c TempK 0.27269E+02 86 0.41023E-03 0.31895E-02 0.15918E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17203 0.19722 1.9258e-005 1.9258e-005 v Velocity[Y] -0.24588 0.93325 0.010714 0.010714 v Velocity[Z] -6.3037e-014 5.3225e-014 -1.5027e-016 -1.5027e-016 v ǁVelocityǁ 0.00013059 0.93338 0.052913 0.052913 v Pressure -0.99969 1.0067 -1.2612e-015 -6.8305e-016 v TempK 295.63 303.18 297.33 297.33 v Density 1 1 1 1 v CourantNb 0.52415 8 7.4901 7.4901 v FourierNb 0.17691 10 1.3202 1.3202 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38141 25.499 2.8563 2.8563 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.57 303.24 297.36 297.35 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81951 17.996 8.8103 8.8103 INSTANT 0.364000000E+02 TIME STEP NUMBER 364 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.78036E-03 0.42287E-01 Friction velocity uk : 0.78036E-03 0.42287E-01 Dimensionless distance yplus : 0.26652E+00 0.14442E+02 Friction thermal sca. tstar : -0.65439E+01 0.76572E-01 Rough dim-less th. sca. tplus : 0.18922E+00 0.10254E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75329E-04 114 0.27438E+00 0.33378E-02 0.80720E+00 c Velocity[X] 0.53924E-03 c Velocity[Y] 0.27985E-02 c Velocity[Z] 0.47942E-29 c Pressure 0.31236E-03 9 0.14171E-07 0.26716E-01 0.11324E-02 c TempK 0.27461E+02 88 0.31657E-03 0.26700E-02 0.14285E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15987 0.15244 2.9674e-006 2.9674e-006 v Velocity[Y] -0.20706 0.90671 0.010572 0.010572 v Velocity[Z] -6.6974e-014 5.5031e-014 -1.0948e-016 -1.0948e-016 v ǁVelocityǁ 0.00065442 0.91777 0.053055 0.053055 v Pressure -0.99975 1.0081 -2.5313e-015 -1.9407e-015 v TempK 295.67 303.14 297.35 297.35 v Density 1 1 1 1 v CourantNb 0.3028 8 7.5167 7.5167 v FourierNb 0.15054 10 1.3131 1.3131 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34462 28.049 2.8421 2.8421 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.63 303.18 297.37 297.36 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85081 17.92 8.8298 8.8298 INSTANT 0.365000000E+02 TIME STEP NUMBER 365 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.16344E-03 0.41955E-01 Friction velocity uk : 0.16344E-03 0.41955E-01 Dimensionless distance yplus : 0.55820E-01 0.14329E+02 Friction thermal sca. tstar : -0.37058E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.39631E-01 0.10173E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72765E-04 112 0.26691E+00 0.31529E-02 0.77912E+00 c Velocity[X] 0.47407E-03 c Velocity[Y] 0.26788E-02 c Velocity[Z] 0.50209E-29 c Pressure 0.32110E-03 11 0.14979E-07 0.27820E-01 0.12472E-02 c TempK 0.27621E+02 89 0.35076E-03 0.25192E-02 0.13213E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1622 0.17252 1.8149e-005 1.8149e-005 v Velocity[Y] -0.20692 0.91232 0.010697 0.010697 v Velocity[Z] -7.1213e-014 5.5005e-014 -1.4799e-016 -1.4799e-016 v ǁVelocityǁ 0.00019448 0.91249 0.052685 0.052685 v Pressure -0.99962 1.0065 -1.5277e-015 -9.3241e-016 v TempK 295.68 303.14 297.36 297.36 v Density 1 1 1 1 v CourantNb 0.28307 8 7.5451 7.5451 v FourierNb 0.1656 10 1.3006 1.3006 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35596 28.461 2.8128 2.8128 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.67 303.15 297.38 297.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.53628 17.564 8.8457 8.8457 INSTANT 0.366000000E+02 TIME STEP NUMBER 366 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10117E-02 0.41474E-01 Friction velocity uk : 0.10117E-02 0.41474E-01 Dimensionless distance yplus : 0.34553E+00 0.14165E+02 Friction thermal sca. tstar : -0.12824E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.24532E+00 0.10057E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71974E-04 112 0.25752E+00 0.32287E-02 0.75396E+00 c Velocity[X] 0.52993E-03 c Velocity[Y] 0.26988E-02 c Velocity[Z] 0.44902E-29 c Pressure 0.33546E-03 10 0.12104E-07 0.29408E-01 0.10859E-02 c TempK 0.27507E+02 89 0.31011E-03 0.30235E-02 0.14619E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16417 0.19409 6.5829e-006 6.5829e-006 v Velocity[Y] -0.32881 0.8676 0.010759 0.010759 v Velocity[Z] -5.9689e-014 5.6117e-014 -1.1875e-016 -1.1875e-016 v ǁVelocityǁ 0.00046677 0.88028 0.053974 0.053974 v Pressure -0.99968 1.0069 1.1546e-016 6.9389e-016 v TempK 295.7 303.14 297.37 297.37 v Density 1 1 1 1 v CourantNb 0.36095 8 7.4794 7.4794 v FourierNb 0.18216 10 1.3029 1.3029 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39156 21.346 2.8177 2.8177 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.68 303.15 297.4 297.39 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.64002 17.77 8.7823 8.7823 INSTANT 0.367000000E+02 TIME STEP NUMBER 367 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.64416E-03 0.41520E-01 Friction velocity uk : 0.64416E-03 0.41520E-01 Dimensionless distance yplus : 0.22000E+00 0.14180E+02 Friction thermal sca. tstar : -0.66937E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.15620E+00 0.10068E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.78876E-04 111 0.27516E+00 0.37736E-02 0.87870E+00 c Velocity[X] 0.60736E-03 c Velocity[Y] 0.31663E-02 c Velocity[Z] 0.59498E-29 c Pressure 0.32013E-03 10 0.14202E-07 0.28146E-01 0.12142E-02 c TempK 0.27896E+02 88 0.36780E-03 0.31776E-02 0.15635E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15045 0.20207 4.2705e-006 4.2705e-006 v Velocity[Y] -0.24853 0.96633 0.010328 0.010328 v Velocity[Z] -5.063e-014 5.7784e-014 -1.6243e-016 -1.6243e-016 v ǁVelocityǁ 0.00030714 0.96738 0.053153 0.053153 v Pressure -0.99985 1.0082 -1.1546e-016 4.7705e-016 v TempK 295.74 303.15 297.38 297.38 v Density 1 1 1 1 v CourantNb 0.31616 8 7.5789 7.5789 v FourierNb 0.15874 10 1.3017 1.3017 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33885 22.972 2.8152 2.8152 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.7 303.15 297.41 297.4 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73064 17.992 8.8806 8.8806 INSTANT 0.368000000E+02 TIME STEP NUMBER 368 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.17788E-03 0.41157E-01 Friction velocity uk : 0.17788E-03 0.41157E-01 Dimensionless distance yplus : 0.60751E-01 0.14056E+02 Friction thermal sca. tstar : -0.21065E+02 0.27298E-02 Rough dim-less th. sca. tplus : 0.43132E-01 0.99797E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.78828E-04 110 0.28828E+00 0.33591E-02 0.82849E+00 c Velocity[X] 0.48657E-03 c Velocity[Y] 0.28726E-02 c Velocity[Z] 0.60492E-29 c Pressure 0.31382E-03 10 0.13924E-07 0.26840E-01 0.12762E-02 c TempK 0.27947E+02 87 0.30755E-03 0.20299E-02 0.12712E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16035 0.20515 -4.3235e-006 -4.3235e-006 v Velocity[Y] -0.17354 0.90429 0.010427 0.010427 v Velocity[Z] -5.2543e-014 6.7651e-014 -1.4084e-016 -1.4084e-016 v ǁVelocityǁ 0.00045094 0.90456 0.05237 0.05237 v Pressure -0.9999 1.0068 -1.0392e-015 -4.12e-016 v TempK 295.8 303.26 297.39 297.39 v Density 1 1 1 1 v CourantNb 0.15307 8 7.5404 7.5404 v FourierNb 0.14881 10 1.2907 1.2907 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37273 25.269 2.7912 2.7912 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.74 303.15 297.42 297.41 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.666 17.873 8.831 8.831 INSTANT 0.369000000E+02 TIME STEP NUMBER 369 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.85948E-03 0.41865E-01 Friction velocity uk : 0.85948E-03 0.41865E-01 Dimensionless distance yplus : 0.29354E+00 0.14298E+02 Friction thermal sca. tstar : -0.78691E+01 0.12064E+00 Rough dim-less th. sca. tplus : 0.20841E+00 0.10151E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71940E-04 111 0.27983E+00 0.31393E-02 0.78050E+00 c Velocity[X] 0.54785E-03 c Velocity[Y] 0.25914E-02 c Velocity[Z] 0.50330E-29 c Pressure 0.33584E-03 10 0.15484E-07 0.28514E-01 0.12626E-02 c TempK 0.27727E+02 88 0.37165E-03 0.22822E-02 0.13781E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17211 0.17985 5.3311e-006 5.3311e-006 v Velocity[Y] -0.22346 0.95219 0.010437 0.010437 v Velocity[Z] -5.4407e-014 6.2173e-014 -1.3159e-016 -1.3159e-016 v ǁVelocityǁ 0.00054175 0.95719 0.052564 0.052564 v Pressure -0.99998 1.007 -8.0824e-016 -2.6021e-016 v TempK 295.86 303.27 297.4 297.4 v Density 1 1 1 1 v CourantNb 0.32732 8 7.4611 7.4611 v FourierNb 0.16369 10 1.2997 1.2997 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41001 21.985 2.8085 2.8085 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.8 303.26 297.43 297.42 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.66343 17.739 8.7607 8.7607 INSTANT 0.370000000E+02 TIME STEP NUMBER 370 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11405E-02 0.36375E-01 Friction velocity uk : 0.11405E-02 0.36375E-01 Dimensionless distance yplus : 0.38953E+00 0.12423E+02 Friction thermal sca. tstar : -0.26691E+01 0.16452E+00 Rough dim-less th. sca. tplus : 0.27656E+00 0.88202E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75265E-04 110 0.25915E+00 0.31382E-02 0.78870E+00 c Velocity[X] 0.56593E-03 c Velocity[Y] 0.25722E-02 c Velocity[Z] 0.49074E-29 c Pressure 0.32371E-03 10 0.11970E-07 0.28210E-01 0.12739E-02 c TempK 0.27660E+02 86 0.28400E-03 0.17492E-02 0.11526E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15738 0.20613 -8.5982e-006 -8.5982e-006 v Velocity[Y] -0.25727 0.85273 0.010293 0.010293 v Velocity[Z] -5.3876e-014 5.8233e-014 -1.1891e-016 -1.1891e-016 v ǁVelocityǁ 0.00034975 0.85819 0.051989 0.051989 v Pressure -1 1.0063 -7.9048e-016 -1.9516e-016 v TempK 295.91 303.28 297.41 297.41 v Density 1 1 1 1 v CourantNb 0.35416 8 7.4987 7.4987 v FourierNb 0.18006 10 1.3025 1.3025 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40357 21.346 2.813 2.813 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.86 303.27 297.44 297.43 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.53617 17.778 8.8012 8.8012 INSTANT 0.371000000E+02 TIME STEP NUMBER 371 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.64857E-03 0.39514E-01 Friction velocity uk : 0.64857E-03 0.39514E-01 Dimensionless distance yplus : 0.22150E+00 0.13495E+02 Friction thermal sca. tstar : -0.26241E+01 0.18473E+00 Rough dim-less th. sca. tplus : 0.15726E+00 0.95814E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73166E-04 110 0.26938E+00 0.29522E-02 0.76650E+00 c Velocity[X] 0.51957E-03 c Velocity[Y] 0.24327E-02 c Velocity[Z] 0.46447E-29 c Pressure 0.32726E-03 10 0.11602E-07 0.28079E-01 0.11373E-02 c TempK 0.27423E+02 86 0.33572E-03 0.20006E-02 0.12924E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15297 0.17599 1.1445e-005 1.1445e-005 v Velocity[Y] -0.17498 0.7912 0.010249 0.010249 v Velocity[Z] -5.4758e-014 5.853e-014 -1.3577e-016 -1.3577e-016 v ǁVelocityǁ 0.00093556 0.79128 0.051722 0.051722 v Pressure -1 1.0075 -2.7534e-016 3.4694e-016 v TempK 295.92 303.3 297.42 297.42 v Density 1 1 1 1 v CourantNb 0.32725 8 7.4534 7.4534 v FourierNb 0.19699 10 1.3186 1.3186 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.43009 21.346 2.8478 2.8478 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.91 303.28 297.45 297.44 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0016 17.851 8.772 8.772 INSTANT 0.372000000E+02 TIME STEP NUMBER 372 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.30651E-03 0.39650E-01 Friction velocity uk : 0.30651E-03 0.39650E-01 Dimensionless distance yplus : 0.10468E+00 0.13542E+02 Friction thermal sca. tstar : -0.45937E+01 0.18650E+00 Rough dim-less th. sca. tplus : 0.74322E-01 0.96144E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71915E-04 110 0.23813E+00 0.28500E-02 0.73159E+00 c Velocity[X] 0.50623E-03 c Velocity[Y] 0.23438E-02 c Velocity[Z] 0.45972E-29 c Pressure 0.31045E-03 15 0.11872E-07 0.26592E-01 0.10057E-02 c TempK 0.27185E+02 86 0.26528E-03 0.23738E-02 0.12718E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1531 0.17064 -7.2513e-006 -7.2513e-006 v Velocity[Y] -0.17041 0.83913 0.010277 0.010277 v Velocity[Z] -5.2865e-014 5.8854e-014 -1.193e-016 -1.193e-016 v ǁVelocityǁ 0.00024318 0.84213 0.051843 0.051843 v Pressure -0.99998 1.0058 -1.2168e-015 -6.3968e-016 v TempK 295.92 303.26 297.43 297.43 v Density 1 1 1 1 v CourantNb 0.21545 8 7.4824 7.4824 v FourierNb 0.19581 10 1.3244 1.3244 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.42071 21.346 2.8618 2.8618 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.92 303.3 297.46 297.45 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.55849 17.387 8.8069 8.8069 INSTANT 0.373000000E+02 TIME STEP NUMBER 373 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14503E-03 0.41198E-01 Friction velocity uk : 0.14503E-03 0.41198E-01 Dimensionless distance yplus : 0.49531E-01 0.14070E+02 Friction thermal sca. tstar : -0.39657E+01 0.20022E+00 Rough dim-less th. sca. tplus : 0.35166E-01 0.99897E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71187E-04 111 0.26253E+00 0.30359E-02 0.75908E+00 c Velocity[X] 0.51200E-03 c Velocity[Y] 0.25239E-02 c Velocity[Z] 0.46523E-29 c Pressure 0.29908E-03 10 0.11647E-07 0.24618E-01 0.86938E-03 c TempK 0.27223E+02 86 0.38058E-03 0.31888E-02 0.14624E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16155 0.1428 5.7609e-006 5.7609e-006 v Velocity[Y] -0.18254 0.84514 0.010379 0.010379 v Velocity[Z] -5.7136e-014 6.7684e-014 -1.482e-016 -1.482e-016 v ǁVelocityǁ 0.00046271 0.84726 0.051962 0.051962 v Pressure -0.99995 1.0059 -1.7764e-016 4.7705e-016 v TempK 295.92 303.26 297.44 297.44 v Density 1 1 1 1 v CourantNb 0.43987 8 7.4668 7.4668 v FourierNb 0.17074 10 1.3407 1.3407 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41107 21.346 2.8984 2.8984 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.92 303.26 297.46 297.46 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.87915 17.977 8.8075 8.8075 INSTANT 0.374000000E+02 TIME STEP NUMBER 374 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32601E-03 0.44614E-01 Friction velocity uk : 0.32601E-03 0.44614E-01 Dimensionless distance yplus : 0.11134E+00 0.15237E+02 Friction thermal sca. tstar : -0.41469E+01 0.17745E+00 Rough dim-less th. sca. tplus : 0.79052E-01 0.10818E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73158E-04 113 0.25859E+00 0.31277E-02 0.77936E+00 c Velocity[X] 0.49761E-03 c Velocity[Y] 0.26301E-02 c Velocity[Z] 0.43467E-29 c Pressure 0.29969E-03 9 0.13172E-07 0.24778E-01 0.94515E-03 c TempK 0.27360E+02 86 0.26609E-03 0.30421E-02 0.14980E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15531 0.16044 -2.0413e-005 -2.0413e-005 v Velocity[Y] -0.21574 0.88269 0.010526 0.010526 v Velocity[Z] -5.5751e-014 6.9492e-014 -1.3205e-016 -1.3205e-016 v ǁVelocityǁ 0.00041806 0.88336 0.05197 0.05197 v Pressure -0.99991 1.0065 -8.7041e-016 -2.4937e-016 v TempK 295.94 303.23 297.44 297.44 v Density 1 1 1 1 v CourantNb 0.15243 8 7.4725 7.4725 v FourierNb 0.16854 10 1.3448 1.3448 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40536 21.346 2.9089 2.9089 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.92 303.26 297.47 297.46 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.42553 17.924 8.8173 8.8173 INSTANT 0.375000000E+02 TIME STEP NUMBER 375 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10569E-02 0.44819E-01 Friction velocity uk : 0.10569E-02 0.44819E-01 Dimensionless distance yplus : 0.36096E+00 0.15307E+02 Friction thermal sca. tstar : -0.10084E+02 0.14912E+00 Rough dim-less th. sca. tplus : 0.25627E+00 0.10868E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73736E-04 111 0.26063E+00 0.31273E-02 0.77753E+00 c Velocity[X] 0.51619E-03 c Velocity[Y] 0.26111E-02 c Velocity[Z] 0.42551E-29 c Pressure 0.31573E-03 10 0.13599E-07 0.26810E-01 0.10592E-02 c TempK 0.27302E+02 87 0.31130E-03 0.34052E-02 0.15068E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16865 0.1624 1.2535e-005 1.2535e-005 v Velocity[Y] -0.17036 0.83094 0.010477 0.010477 v Velocity[Z] -5.6172e-014 6.9496e-014 -1.2927e-016 -1.2927e-016 v ǁVelocityǁ 0.00047131 0.83103 0.052041 0.052041 v Pressure -0.99989 1.0085 -1.0036e-015 -4.4452e-016 v TempK 295.98 303.25 297.45 297.45 v Density 1 1 1 1 v CourantNb 0.53879 8 7.4391 7.4391 v FourierNb 0.1854 10 1.3499 1.3499 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40199 22.307 2.9206 2.9206 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.94 303.23 297.48 297.47 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.87135 17.706 8.789 8.789 INSTANT 0.376000000E+02 TIME STEP NUMBER 376 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.61165E-03 0.46231E-01 Friction velocity uk : 0.61165E-03 0.46231E-01 Dimensionless distance yplus : 0.20890E+00 0.15789E+02 Friction thermal sca. tstar : -0.10720E+02 0.15367E+00 Rough dim-less th. sca. tplus : 0.14831E+00 0.11210E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73155E-04 114 0.24640E+00 0.30627E-02 0.77070E+00 c Velocity[X] 0.55249E-03 c Velocity[Y] 0.25102E-02 c Velocity[Z] 0.48348E-29 c Pressure 0.32490E-03 9 0.15395E-07 0.28107E-01 0.10560E-02 c TempK 0.27291E+02 88 0.32202E-03 0.47127E-02 0.17650E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.13708 0.21264 -8.4891e-006 -8.4891e-006 v Velocity[Y] -0.19574 0.81822 0.010397 0.010397 v Velocity[Z] -5.653e-014 6.7066e-014 -1.3767e-016 -1.3767e-016 v ǁVelocityǁ 0.0004062 0.82077 0.052183 0.052183 v Pressure -0.99982 1.0065 -7.6383e-016 -1.4095e-016 v TempK 296.02 303.24 297.46 297.46 v Density 1 1 1 1 v CourantNb 0.45186 8 7.4389 7.4389 v FourierNb 0.15372 10 1.3503 1.3503 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39435 22.993 2.9212 2.9212 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.98 303.25 297.49 297.48 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0757 17.484 8.7892 8.7892 INSTANT 0.377000000E+02 TIME STEP NUMBER 377 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.35315E-03 0.42270E-01 Friction velocity uk : 0.35315E-03 0.42270E-01 Dimensionless distance yplus : 0.12061E+00 0.14436E+02 Friction thermal sca. tstar : -0.29841E+01 0.16464E+00 Rough dim-less th. sca. tplus : 0.85632E-01 0.10250E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73274E-04 113 0.27080E+00 0.30118E-02 0.75838E+00 c Velocity[X] 0.53315E-03 c Velocity[Y] 0.24786E-02 c Velocity[Z] 0.49270E-29 c Pressure 0.31378E-03 10 0.14605E-07 0.27422E-01 0.10920E-02 c TempK 0.27353E+02 89 0.35674E-03 0.42455E-02 0.17053E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19927 0.18277 1.5688e-005 1.5688e-005 v Velocity[Y] -0.18181 0.80253 0.010368 0.010368 v Velocity[Z] -5.6852e-014 6.0846e-014 -1.4299e-016 -1.4299e-016 v ǁVelocityǁ 0.00072455 0.80814 0.052209 0.052209 v Pressure -0.99974 1.0061 -1.3856e-015 -7.6978e-016 v TempK 296.03 303.3 297.47 297.47 v Density 1 1 1 1 v CourantNb 0.79493 8 7.4804 7.4804 v FourierNb 0.14327 10 1.348 1.348 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39661 22.166 2.9157 2.9157 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.02 303.24 297.5 297.49 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.3533 17.566 8.8284 8.8284 INSTANT 0.378000000E+02 TIME STEP NUMBER 378 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.79106E-03 0.41657E-01 Friction velocity uk : 0.79106E-03 0.41657E-01 Dimensionless distance yplus : 0.27017E+00 0.14227E+02 Friction thermal sca. tstar : -0.27038E+01 0.17030E+00 Rough dim-less th. sca. tplus : 0.19182E+00 0.10101E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70416E-04 115 0.25918E+00 0.30867E-02 0.76759E+00 c Velocity[X] 0.48725E-03 c Velocity[Y] 0.25994E-02 c Velocity[Z] 0.47599E-29 c Pressure 0.31713E-03 10 0.15389E-07 0.29112E-01 0.11560E-02 c TempK 0.27539E+02 90 0.28307E-03 0.45839E-02 0.17193E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16142 0.16322 -9.4454e-007 -9.4454e-007 v Velocity[Y] -0.18446 0.80128 0.010451 0.010451 v Velocity[Z] -5.5385e-014 5.4923e-014 -1.1181e-016 -1.1181e-016 v ǁVelocityǁ 0.00011156 0.80322 0.05248 0.05248 v Pressure -0.99973 1.0076 -8.793e-016 -1.5179e-016 v TempK 296.02 303.25 297.48 297.48 v Density 1 1 1 1 v CourantNb 0.23101 8 7.4548 7.4548 v FourierNb 0.15759 10 1.3324 1.3324 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39595 21.346 2.8825 2.8825 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.03 303.3 297.5 297.5 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.58308 16.976 8.7872 8.7872 INSTANT 0.379000000E+02 TIME STEP NUMBER 379 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28089E-03 0.43958E-01 Friction velocity uk : 0.28089E-03 0.43958E-01 Dimensionless distance yplus : 0.95934E-01 0.15013E+02 Friction thermal sca. tstar : -0.89212E+01 0.17636E+00 Rough dim-less th. sca. tplus : 0.68112E-01 0.10659E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70601E-04 115 0.25219E+00 0.29036E-02 0.73182E+00 c Velocity[X] 0.52791E-03 c Velocity[Y] 0.23757E-02 c Velocity[Z] 0.50632E-29 c Pressure 0.32666E-03 11 0.16307E-07 0.31461E-01 0.11236E-02 c TempK 0.27564E+02 91 0.30435E-03 0.42862E-02 0.17201E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17451 0.16085 7.271e-006 7.271e-006 v Velocity[Y] -0.19148 0.85689 0.010571 0.010571 v Velocity[Z] -5.7296e-014 5.5778e-014 -1.3347e-016 -1.3347e-016 v ǁVelocityǁ 0.00040983 0.86102 0.052464 0.052464 v Pressure -0.99971 1.0068 -6.2172e-017 5.6379e-016 v TempK 295.99 303.27 297.49 297.49 v Density 1 1 1 1 v CourantNb 0.36043 8 7.4335 7.4335 v FourierNb 0.17335 10 1.328 1.328 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38679 21.346 2.8755 2.8755 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.02 303.25 297.52 297.51 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.65626 17.965 8.7615 8.7615 INSTANT 0.380000000E+02 TIME STEP NUMBER 380 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.62274E-03 0.43239E-01 Friction velocity uk : 0.62274E-03 0.43239E-01 Dimensionless distance yplus : 0.21269E+00 0.14768E+02 Friction thermal sca. tstar : -0.12488E+02 0.11910E+00 Rough dim-less th. sca. tplus : 0.15100E+00 0.10485E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71743E-04 116 0.27460E+00 0.27431E-02 0.70001E+00 c Velocity[X] 0.50159E-03 c Velocity[Y] 0.22415E-02 c Velocity[Z] 0.49435E-29 c Pressure 0.32907E-03 10 0.17523E-07 0.33397E-01 0.11371E-02 c TempK 0.27556E+02 92 0.27519E-03 0.46434E-02 0.17755E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15475 0.17593 -5.1221e-006 -5.1221e-006 v Velocity[Y] -0.20333 0.8838 0.010502 0.010502 v Velocity[Z] -6.3323e-014 5.1011e-014 -1.2181e-016 -1.2181e-016 v ǁVelocityǁ 6.6946e-005 0.89079 0.0526 0.0526 v Pressure -0.9997 1.0062 -5.3291e-017 5.7463e-016 v TempK 295.97 303.28 297.5 297.5 v Density 1 1 1 1 v CourantNb 0.27497 8 7.4291 7.4291 v FourierNb 0.18698 10 1.3219 1.3219 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39912 21.346 2.8635 2.8635 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.99 303.27 297.53 297.52 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.68036 17.79 8.7509 8.7509 INSTANT 0.381000000E+02 TIME STEP NUMBER 381 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.41407E-03 0.41669E-01 Friction velocity uk : 0.41407E-03 0.41669E-01 Dimensionless distance yplus : 0.14142E+00 0.14231E+02 Friction thermal sca. tstar : -0.41198E+01 0.51519E+00 Rough dim-less th. sca. tplus : 0.10040E+00 0.10104E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69979E-04 114 0.25681E+00 0.27669E-02 0.69343E+00 c Velocity[X] 0.49047E-03 c Velocity[Y] 0.22764E-02 c Velocity[Z] 0.51808E-29 c Pressure 0.34270E-03 9 0.17448E-07 0.35244E-01 0.10930E-02 c TempK 0.27457E+02 92 0.27920E-03 0.41095E-02 0.17015E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16029 0.15949 9.3939e-006 9.3939e-006 v Velocity[Y] -0.20146 0.84083 0.010641 0.010641 v Velocity[Z] -6.6428e-014 5.6833e-014 -1.3207e-016 -1.3207e-016 v ǁVelocityǁ 0.00017248 0.85344 0.052532 0.052532 v Pressure -0.99967 1.0057 -2.931e-016 2.8189e-016 v TempK 295.99 303.29 297.52 297.52 v Density 1 1 1 1 v CourantNb 0.31243 8 7.4247 7.4247 v FourierNb 0.18752 10 1.3249 1.3249 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40028 21.346 2.8697 2.8697 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.97 303.28 297.54 297.53 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1574 17.793 8.7496 8.7496 INSTANT 0.382000000E+02 TIME STEP NUMBER 382 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11372E-03 0.43889E-01 Friction velocity uk : 0.11372E-03 0.43889E-01 Dimensionless distance yplus : 0.38837E-01 0.14989E+02 Friction thermal sca. tstar : -0.64809E+01 0.33543E+00 Rough dim-less th. sca. tplus : 0.27574E-01 0.10642E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72494E-04 112 0.25041E+00 0.28808E-02 0.69034E+00 c Velocity[X] 0.52576E-03 c Velocity[Y] 0.23550E-02 c Velocity[Z] 0.49250E-29 c Pressure 0.34903E-03 10 0.17417E-07 0.36638E-01 0.11179E-02 c TempK 0.27361E+02 90 0.27961E-03 0.39473E-02 0.16459E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17323 0.19039 -4.6314e-006 -4.6314e-006 v Velocity[Y] -0.22024 0.94804 0.010891 0.010891 v Velocity[Z] -6.3563e-014 5.9778e-014 -1.3872e-016 -1.3872e-016 v ǁVelocityǁ 0.00036189 0.94817 0.052617 0.052617 v Pressure -0.99965 1.0078 -1.2434e-015 -6.9389e-016 v TempK 296.02 303.31 297.53 297.53 v Density 1 1 1 1 v CourantNb 0.45936 8 7.3828 7.3828 v FourierNb 0.18535 10 1.3288 1.3288 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40808 21.346 2.8799 2.8799 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.99 303.29 297.55 297.55 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.1436 16.85 8.7117 8.7117 INSTANT 0.383000000E+02 TIME STEP NUMBER 383 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.27158E-03 0.40346E-01 Friction velocity uk : 0.27158E-03 0.40346E-01 Dimensionless distance yplus : 0.92753E-01 0.13779E+02 Friction thermal sca. tstar : -0.35847E+01 0.24727E+00 Rough dim-less th. sca. tplus : 0.65853E-01 0.97831E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74275E-04 114 0.25927E+00 0.33608E-02 0.79021E+00 c Velocity[X] 0.56921E-03 c Velocity[Y] 0.27916E-02 c Velocity[Z] 0.55091E-29 c Pressure 0.34559E-03 10 0.17632E-07 0.36081E-01 0.12052E-02 c TempK 0.27549E+02 89 0.33666E-03 0.38944E-02 0.16085E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18768 0.16864 3.3643e-005 3.3643e-005 v Velocity[Y] -0.22952 1.1038 0.010724 0.010724 v Velocity[Z] -5.2932e-014 6.0497e-014 -1.4028e-016 -1.4028e-016 v ǁVelocityǁ 6.2249e-005 1.1052 0.052364 0.052364 v Pressure -0.99965 1.0075 -1.2612e-015 -7.8063e-016 v TempK 296.04 303.29 297.55 297.55 v Density 1 1 1 1 v CourantNb 0.3848 8 7.305 7.305 v FourierNb 0.15744 10 1.3433 1.3433 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37413 22.65 2.913 2.913 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.02 303.31 297.57 297.56 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75917 17.886 8.6484 8.6484 INSTANT 0.384000000E+02 TIME STEP NUMBER 384 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.43704E-03 0.44208E-01 Friction velocity uk : 0.43704E-03 0.44208E-01 Dimensionless distance yplus : 0.14926E+00 0.15098E+02 Friction thermal sca. tstar : -0.23463E+01 0.20220E+00 Rough dim-less th. sca. tplus : 0.10597E+00 0.10720E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74151E-04 113 0.27179E+00 0.29990E-02 0.74094E+00 c Velocity[X] 0.52174E-03 c Velocity[Y] 0.24772E-02 c Velocity[Z] 0.49432E-29 c Pressure 0.32272E-03 10 0.18560E-07 0.33138E-01 0.12657E-02 c TempK 0.27609E+02 89 0.25757E-03 0.37582E-02 0.16807E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21109 0.15616 4.3391e-007 4.3391e-007 v Velocity[Y] -0.22014 1.1109 0.010653 0.010653 v Velocity[Z] -5.6531e-014 5.8716e-014 -1.4469e-016 -1.4469e-016 v ǁVelocityǁ 0.00045565 1.1139 0.051293 0.051293 v Pressure -1.0004 1.0063 1.3323e-016 7.481e-016 v TempK 296.04 303.22 297.57 297.57 v Density 1 1 1 1 v CourantNb 0.3267 8 7.2996 7.2996 v FourierNb 0.16401 9.4601 1.3564 1.3564 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41155 24.915 2.9442 2.9442 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.04 303.29 297.59 297.58 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.6607 17.274 8.656 8.656 INSTANT 0.385000000E+02 TIME STEP NUMBER 385 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.55331E-03 0.38655E-01 Friction velocity uk : 0.55331E-03 0.38655E-01 Dimensionless distance yplus : 0.18897E+00 0.13202E+02 Friction thermal sca. tstar : -0.35712E+01 0.12234E+00 Rough dim-less th. sca. tplus : 0.13417E+00 0.93730E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72533E-04 113 0.26592E+00 0.31884E-02 0.75674E+00 c Velocity[X] 0.56073E-03 c Velocity[Y] 0.26277E-02 c Velocity[Z] 0.54317E-29 c Pressure 0.35128E-03 10 0.18732E-07 0.34961E-01 0.12975E-02 c TempK 0.27436E+02 88 0.35265E-03 0.35474E-02 0.16610E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23682 0.16164 2.397e-005 2.397e-005 v Velocity[Y] -0.18938 0.88405 0.010644 0.010644 v Velocity[Z] -5.8956e-014 5.832e-014 -1.2608e-016 -1.2608e-016 v ǁVelocityǁ 0.00042533 0.90694 0.051289 0.051289 v Pressure -1.0011 1.0099 -5.862e-016 1.0842e-017 v TempK 296.02 303.19 297.58 297.58 v Density 1 1 1 1 v CourantNb 0.16452 8 7.1559 7.1559 v FourierNb 0.17822 10 1.3702 1.3702 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.42727 27.407 2.9758 2.9758 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.04 303.22 297.6 297.6 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.7019 17.888 8.5261 8.5261 INSTANT 0.386000000E+02 TIME STEP NUMBER 386 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.43639E-03 0.45844E-01 Friction velocity uk : 0.43639E-03 0.45844E-01 Dimensionless distance yplus : 0.14904E+00 0.15657E+02 Friction thermal sca. tstar : -0.48024E+01 0.57086E-01 Rough dim-less th. sca. tplus : 0.10582E+00 0.11116E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74885E-04 114 0.28122E+00 0.33525E-02 0.80513E+00 c Velocity[X] 0.62223E-03 c Velocity[Y] 0.27302E-02 c Velocity[Z] 0.55139E-29 c Pressure 0.35290E-03 14 0.15742E-07 0.32858E-01 0.13361E-02 c TempK 0.27502E+02 88 0.34112E-03 0.41413E-02 0.17337E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15745 0.16212 -7.8259e-006 -7.8259e-006 v Velocity[Y] -0.17391 0.94265 0.010457 0.010457 v Velocity[Z] -5.7683e-014 5.6025e-014 -1.4591e-016 -1.4591e-016 v ǁVelocityǁ 0.00024169 0.94591 0.050735 0.050735 v Pressure -1.0015 1.0079 1.8652e-016 7.0473e-016 v TempK 295.99 303.16 297.59 297.59 v Density 1 1 1 1 v CourantNb 0.31549 8 7.1449 7.1449 v FourierNb 0.15689 10 1.3934 1.3934 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39394 28.461 3.0262 3.0262 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.02 303.19 297.62 297.61 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57018 17.832 8.5383 8.5383 INSTANT 0.387000000E+02 TIME STEP NUMBER 387 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.21591E-03 0.41554E-01 Friction velocity uk : 0.21591E-03 0.41554E-01 Dimensionless distance yplus : 0.73738E-01 0.14192E+02 Friction thermal sca. tstar : -0.59453E+01 0.15405E-01 Rough dim-less th. sca. tplus : 0.52353E-01 0.10076E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73189E-04 109 0.25810E+00 0.32054E-02 0.78171E+00 c Velocity[X] 0.57892E-03 c Velocity[Y] 0.26264E-02 c Velocity[Z] 0.50889E-29 c Pressure 0.35034E-03 10 0.17761E-07 0.31467E-01 0.14451E-02 c TempK 0.27507E+02 88 0.36381E-03 0.38783E-02 0.16127E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14576 0.1673 2.1352e-005 2.1352e-005 v Velocity[Y] -0.19391 0.88335 0.010447 0.010447 v Velocity[Z] -5.7451e-014 5.627e-014 -1.341e-016 -1.341e-016 v ǁVelocityǁ 0.00020213 0.88602 0.051101 0.051101 v Pressure -1.0011 1.009 -1.7497e-015 -1.0734e-015 v TempK 295.97 303.13 297.61 297.61 v Density 1 1 1 1 v CourantNb 0.44453 8 7.0779 7.0779 v FourierNb 0.16754 10 1.4092 1.4092 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38388 21.882 3.0595 3.0595 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.99 303.16 297.63 297.62 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75116 17.826 8.4871 8.4871 INSTANT 0.388000000E+02 TIME STEP NUMBER 388 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.65009E-03 0.43258E-01 Friction velocity uk : 0.65009E-03 0.43258E-01 Dimensionless distance yplus : 0.22202E+00 0.14774E+02 Friction thermal sca. tstar : -0.39904E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.15763E+00 0.10489E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71034E-04 111 0.26897E+00 0.31679E-02 0.78576E+00 c Velocity[X] 0.51504E-03 c Velocity[Y] 0.26529E-02 c Velocity[Z] 0.53134E-29 c Pressure 0.32576E-03 11 0.17202E-07 0.28400E-01 0.12262E-02 c TempK 0.27717E+02 91 0.37397E-03 0.43133E-02 0.18093E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15311 0.1616 5.383e-007 5.383e-007 v Velocity[Y] -0.22892 0.89155 0.010627 0.010627 v Velocity[Z] -4.8525e-014 5.8755e-014 -1.3705e-016 -1.3705e-016 v ǁVelocityǁ 8.8661e-005 0.89243 0.051111 0.051111 v Pressure -1.0004 1.007 4.4409e-016 9.9747e-016 v TempK 295.99 302.98 297.62 297.62 v Density 1 1 1 1 v CourantNb 0.33522 8 7.174 7.174 v FourierNb 0.15778 10 1.4137 1.4137 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.33678 24.071 3.0678 3.0678 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.97 303.15 297.65 297.64 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.60685 17.636 8.5877 8.5877 INSTANT 0.389000000E+02 TIME STEP NUMBER 389 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32943E-03 0.41059E-01 Friction velocity uk : 0.32943E-03 0.41059E-01 Dimensionless distance yplus : 0.11251E+00 0.14023E+02 Friction thermal sca. tstar : -0.61847E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.79881E-01 0.99560E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72967E-04 116 0.27018E+00 0.30827E-02 0.75911E+00 c Velocity[X] 0.53234E-03 c Velocity[Y] 0.25504E-02 c Velocity[Z] 0.57010E-29 c Pressure 0.34347E-03 11 0.18992E-07 0.31269E-01 0.12093E-02 c TempK 0.27751E+02 90 0.35928E-03 0.41087E-02 0.16661E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16836 0.15537 1.7732e-005 1.7732e-005 v Velocity[Y] -0.24547 0.96052 0.010683 0.010683 v Velocity[Z] -5.4657e-014 5.4189e-014 -1.3404e-016 -1.3404e-016 v ǁVelocityǁ 0.00020346 0.96057 0.051073 0.051073 v Pressure -0.99983 1.0076 -1.8119e-015 -1.1276e-015 v TempK 296.02 302.99 297.64 297.64 v Density 1 1 1 1 v CourantNb 0.19227 8 7.2296 7.2296 v FourierNb 0.16108 10 1.3812 1.3812 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37046 21.346 2.9943 2.9943 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.99 303.15 297.66 297.65 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.40609 16.862 8.6108 8.6108 INSTANT 0.390000000E+02 TIME STEP NUMBER 390 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.43732E-03 0.44224E-01 Friction velocity uk : 0.43732E-03 0.44224E-01 Dimensionless distance yplus : 0.14936E+00 0.15104E+02 Friction thermal sca. tstar : -0.80216E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.10604E+00 0.10724E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73091E-04 112 0.27069E+00 0.31378E-02 0.76794E+00 c Velocity[X] 0.58492E-03 c Velocity[Y] 0.25528E-02 c Velocity[Z] 0.54620E-29 c Pressure 0.34651E-03 10 0.14244E-07 0.30747E-01 0.12217E-02 c TempK 0.27629E+02 90 0.34289E-03 0.44509E-02 0.16943E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21182 0.15551 -5.9337e-006 -5.9337e-006 v Velocity[Y] -0.2737 0.83352 0.010609 0.010609 v Velocity[Z] -5.2494e-014 5.3252e-014 -1.1353e-016 -1.1353e-016 v ǁVelocityǁ 0.00042767 0.83554 0.051209 0.051209 v Pressure -1.0001 1.0081 -1.4388e-015 -8.5652e-016 v TempK 296.04 303 297.65 297.65 v Density 1 1 1 1 v CourantNb 0.35734 8 7.2248 7.2248 v FourierNb 0.16976 10 1.3665 1.3665 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39237 21.346 2.963 2.963 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.02 303.15 297.67 297.66 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.65116 17.929 8.5913 8.5913 INSTANT 0.391000000E+02 TIME STEP NUMBER 391 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.60636E-03 0.41070E-01 Friction velocity uk : 0.60636E-03 0.41070E-01 Dimensionless distance yplus : 0.20709E+00 0.14027E+02 Friction thermal sca. tstar : -0.45167E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.14703E+00 0.99586E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74061E-04 114 0.26435E+00 0.34154E-02 0.82177E+00 c Velocity[X] 0.60374E-03 c Velocity[Y] 0.28117E-02 c Velocity[Z] 0.52895E-29 c Pressure 0.31895E-03 10 0.14700E-07 0.28355E-01 0.12419E-02 c TempK 0.27543E+02 90 0.38455E-03 0.49533E-02 0.17552E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1643 0.16152 1.0872e-005 1.0872e-005 v Velocity[Y] -0.24236 1.1183 0.010321 0.010321 v Velocity[Z] -4.9541e-014 5.6324e-014 -1.3132e-016 -1.3132e-016 v ǁVelocityǁ 0.00016333 1.1192 0.051287 0.051287 v Pressure -1.0004 1.0092 3.4639e-016 8.3484e-016 v TempK 296.04 302.99 297.67 297.67 v Density 1 1 1 1 v CourantNb 0.37754 8 7.259 7.259 v FourierNb 0.17213 10 1.3544 1.3544 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36741 21.346 2.9346 2.9346 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.04 303.15 297.68 297.68 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.92877 17.663 8.6135 8.6135 INSTANT 0.392000000E+02 TIME STEP NUMBER 392 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.66954E-03 0.43952E-01 Friction velocity uk : 0.66954E-03 0.43952E-01 Dimensionless distance yplus : 0.22867E+00 0.15011E+02 Friction thermal sca. tstar : -0.42039E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.16235E+00 0.10658E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77455E-04 113 0.27011E+00 0.35127E-02 0.84649E+00 c Velocity[X] 0.56621E-03 c Velocity[Y] 0.29465E-02 c Velocity[Z] 0.59597E-29 c Pressure 0.30228E-03 11 0.15938E-07 0.26672E-01 0.11328E-02 c TempK 0.27570E+02 90 0.35236E-03 0.48423E-02 0.17426E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18945 0.16674 -9.7582e-006 -9.7582e-006 v Velocity[Y] -0.26953 0.79913 0.010332 0.010332 v Velocity[Z] -5.6868e-014 5.1253e-014 -1.3924e-016 -1.3924e-016 v ǁVelocityǁ 0.00045166 0.80576 0.051369 0.051369 v Pressure -1.001 1.0089 -4.885e-016 8.6736e-017 v TempK 296.02 302.98 297.69 297.69 v Density 1 1 1 1 v CourantNb 0.28772 8 7.2815 7.2815 v FourierNb 0.14837 10 1.3421 1.3421 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39876 22.941 2.9075 2.9075 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.04 303.15 297.71 297.7 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.73125 17.37 8.6236 8.6236 INSTANT 0.393000000E+02 TIME STEP NUMBER 393 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.51473E-03 0.40181E-01 Friction velocity uk : 0.51473E-03 0.40181E-01 Dimensionless distance yplus : 0.17580E+00 0.13723E+02 Friction thermal sca. tstar : -0.48726E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.12481E+00 0.97430E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73761E-04 113 0.26088E+00 0.32427E-02 0.81504E+00 c Velocity[X] 0.54186E-03 c Velocity[Y] 0.27008E-02 c Velocity[Z] 0.58690E-29 c Pressure 0.31032E-03 10 0.17338E-07 0.27119E-01 0.12427E-02 c TempK 0.27605E+02 88 0.38756E-03 0.44306E-02 0.15560E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17004 0.15131 1.1548e-005 1.1548e-005 v Velocity[Y] -0.24811 0.9059 0.010296 0.010296 v Velocity[Z] -6.6595e-014 5.4308e-014 -1.4535e-016 -1.4535e-016 v ǁVelocityǁ 0.00014883 0.90601 0.050638 0.050638 v Pressure -1.0015 1.0064 -1.8563e-015 -1.301e-015 v TempK 295.99 302.96 297.71 297.71 v Density 1 1 1 1 v CourantNb 0.11038 8 7.284 7.284 v FourierNb 0.16109 10 1.3212 1.3212 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34386 25.235 2.8616 2.8616 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.02 303.15 297.73 297.72 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.31223 17.753 8.6052 8.6052 INSTANT 0.394000000E+02 TIME STEP NUMBER 394 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.63040E-03 0.43994E-01 Friction velocity uk : 0.63040E-03 0.43994E-01 Dimensionless distance yplus : 0.21530E+00 0.15025E+02 Friction thermal sca. tstar : -0.56102E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.15286E+00 0.10668E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72238E-04 112 0.26391E+00 0.31289E-02 0.78944E+00 c Velocity[X] 0.53196E-03 c Velocity[Y] 0.25969E-02 c Velocity[Z] 0.46615E-29 c Pressure 0.32264E-03 10 0.11885E-07 0.27686E-01 0.10699E-02 c TempK 0.27261E+02 87 0.33136E-03 0.46741E-02 0.16354E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16436 0.18128 -5.8868e-007 -5.8868e-007 v Velocity[Y] -0.27499 0.84546 0.010345 0.010345 v Velocity[Z] -6.6955e-014 5.3173e-014 -1.3613e-016 -1.3613e-016 v ǁVelocityǁ 0.00038053 0.84709 0.050743 0.050743 v Pressure -1.0019 1.007 -2.6912e-015 -2.0166e-015 v TempK 295.98 302.97 297.73 297.73 v Density 1 1 1 1 v CourantNb 0.28801 8 7.2406 7.2406 v FourierNb 0.1772 10 1.3244 1.3244 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37825 27.759 2.8673 2.8673 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.99 303.15 297.75 297.74 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.99048 17.887 8.565 8.565 INSTANT 0.395000000E+02 TIME STEP NUMBER 395 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.66526E-03 0.40731E-01 Friction velocity uk : 0.66526E-03 0.40731E-01 Dimensionless distance yplus : 0.22721E+00 0.13911E+02 Friction thermal sca. tstar : -0.77759E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.16131E+00 0.98764E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71105E-04 111 0.26562E+00 0.30178E-02 0.76210E+00 c Velocity[X] 0.55020E-03 c Velocity[Y] 0.24676E-02 c Velocity[Z] 0.45868E-29 c Pressure 0.31306E-03 9 0.13776E-07 0.26773E-01 0.10580E-02 c TempK 0.27011E+02 88 0.34550E-03 0.54791E-02 0.17805E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19448 0.16133 1.1319e-005 1.1319e-005 v Velocity[Y] -0.20588 0.89882 0.01052 0.01052 v Velocity[Z] -6.3717e-014 5.4992e-014 -1.4599e-016 -1.4599e-016 v ǁVelocityǁ 0.00018985 0.89911 0.050397 0.050397 v Pressure -1.0024 1.0062 1.1724e-015 1.7998e-015 v TempK 296 303 297.75 297.75 v Density 1 1 1 1 v CourantNb 0.37307 8 7.2684 7.2684 v FourierNb 0.18468 10 1.3303 1.3303 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41607 27.642 2.8772 2.8772 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.98 303.15 297.76 297.76 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.66358 17.245 8.5986 8.5986 INSTANT 0.396000000E+02 TIME STEP NUMBER 396 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.76558E-03 0.44446E-01 Friction velocity uk : 0.76558E-03 0.44446E-01 Dimensionless distance yplus : 0.26147E+00 0.15180E+02 Friction thermal sca. tstar : -0.35314E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.18564E+00 0.10777E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70848E-04 111 0.25432E+00 0.31089E-02 0.76690E+00 c Velocity[X] 0.54789E-03 c Velocity[Y] 0.25610E-02 c Velocity[Z] 0.50424E-29 c Pressure 0.32728E-03 10 0.16498E-07 0.28657E-01 0.10850E-02 c TempK 0.26751E+02 90 0.28265E-03 0.62860E-02 0.17994E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17719 0.15267 8.4978e-006 8.4978e-006 v Velocity[Y] -0.34991 1.145 0.010528 0.010528 v Velocity[Z] -6.0659e-014 5.2238e-014 -1.2996e-016 -1.2996e-016 v ǁVelocityǁ 0.00058382 1.1471 0.050319 0.050319 v Pressure -1.0028 1.0065 -3.6415e-016 2.3852e-016 v TempK 296.04 303.01 297.76 297.76 v Density 1 1 1 1 v CourantNb 0.44292 8 7.2797 7.2797 v FourierNb 0.15534 10 1.3306 1.3306 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41083 28.461 2.8769 2.8769 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296 303.15 297.78 297.77 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.87968 17.527 8.6104 8.6104 INSTANT 0.397000000E+02 TIME STEP NUMBER 397 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.52572E-03 0.39343E-01 Friction velocity uk : 0.52572E-03 0.39343E-01 Dimensionless distance yplus : 0.17955E+00 0.13437E+02 Friction thermal sca. tstar : -0.34614E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.12748E+00 0.95398E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72877E-04 112 0.26123E+00 0.31814E-02 0.78565E+00 c Velocity[X] 0.59222E-03 c Velocity[Y] 0.25891E-02 c Velocity[Z] 0.48911E-29 c Pressure 0.34076E-03 10 0.14321E-07 0.30235E-01 0.11490E-02 c TempK 0.26629E+02 91 0.42142E-03 0.57946E-02 0.18168E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19434 0.2085 1.7304e-005 1.7304e-005 v Velocity[Y] -0.23963 0.88843 0.010545 0.010545 v Velocity[Z] -5.6049e-014 5.399e-014 -1.4448e-016 -1.4448e-016 v ǁVelocityǁ 0.00031131 0.89317 0.050559 0.050559 v Pressure -1.0031 1.007 -8.4377e-016 -2.4937e-016 v TempK 296.06 303 297.77 297.77 v Density 1 1 1 1 v CourantNb 0.44463 8 7.2497 7.2497 v FourierNb 0.16937 10 1.3353 1.3353 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38136 21.346 2.885 2.885 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.04 303.15 297.79 297.79 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0395 17.836 8.585 8.585 INSTANT 0.398000000E+02 TIME STEP NUMBER 398 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.78903E-03 0.42969E-01 Friction velocity uk : 0.78903E-03 0.42969E-01 Dimensionless distance yplus : 0.26948E+00 0.14675E+02 Friction thermal sca. tstar : -0.43788E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.19133E+00 0.10419E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72907E-04 112 0.25233E+00 0.33398E-02 0.80388E+00 c Velocity[X] 0.59222E-03 c Velocity[Y] 0.27476E-02 c Velocity[Z] 0.49765E-29 c Pressure 0.30425E-03 10 0.13980E-07 0.26868E-01 0.10590E-02 c TempK 0.26609E+02 91 0.29015E-03 0.64943E-02 0.20058E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16642 0.1486 -5.4154e-008 -5.4154e-008 v Velocity[Y] -0.23461 1.0878 0.010401 0.010401 v Velocity[Z] -5.3954e-014 5.6118e-014 -1.5272e-016 -1.5272e-016 v ǁVelocityǁ 0.00024216 1.0878 0.050616 0.050616 v Pressure -1.0032 1.006 -5.7732e-016 7.5894e-017 v TempK 296.05 303.01 297.78 297.78 v Density 1 1 1 1 v CourantNb 0.41365 8 7.3179 7.3179 v FourierNb 0.16551 10 1.3312 1.3312 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41885 23.362 2.8771 2.8771 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.06 303.15 297.8 297.8 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.98981 17.454 8.6491 8.6491 INSTANT 0.399000000E+02 TIME STEP NUMBER 399 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.74633E-03 0.37758E-01 Friction velocity uk : 0.74633E-03 0.37758E-01 Dimensionless distance yplus : 0.25489E+00 0.12896E+02 Friction thermal sca. tstar : -0.68013E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.18097E+00 0.91556E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73349E-04 114 0.26222E+00 0.35689E-02 0.87426E+00 c Velocity[X] 0.57422E-03 c Velocity[Y] 0.29947E-02 c Velocity[Z] 0.51694E-29 c Pressure 0.30825E-03 10 0.14860E-07 0.27416E-01 0.12009E-02 c TempK 0.26875E+02 90 0.40763E-03 0.58355E-02 0.18931E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18499 0.15872 2.7179e-006 2.7179e-006 v Velocity[Y] -0.23685 0.99905 0.010329 0.010329 v Velocity[Z] -5.6047e-014 5.7189e-014 -1.2619e-016 -1.2619e-016 v ǁVelocityǁ 0.00051103 0.99905 0.050339 0.050339 v Pressure -1.0027 1.0085 -5.862e-016 -4.3368e-017 v TempK 296.01 303.13 297.8 297.8 v Density 1 1 1 1 v CourantNb 0.049588 8 7.3203 7.3203 v FourierNb 0.15841 10 1.328 1.328 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34741 21.346 2.869 2.869 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.05 303.15 297.82 297.81 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.74196 17.632 8.6482 8.6482 INSTANT 0.400000000E+02 TIME STEP NUMBER 400 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.20509E-03 0.42367E-01 Friction velocity uk : 0.20509E-03 0.42367E-01 Dimensionless distance yplus : 0.70043E-01 0.14470E+02 Friction thermal sca. tstar : -0.56604E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.49729E-01 0.10273E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74808E-04 111 0.26580E+00 0.31716E-02 0.80515E+00 c Velocity[X] 0.56831E-03 c Velocity[Y] 0.26033E-02 c Velocity[Z] 0.49815E-29 c Pressure 0.30873E-03 10 0.14692E-07 0.28873E-01 0.11025E-02 c TempK 0.26841E+02 90 0.25307E-03 0.54782E-02 0.19040E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18511 0.15992 -2.2297e-005 -2.2297e-005 v Velocity[Y] -0.18938 0.88612 0.010293 0.010293 v Velocity[Z] -5.3287e-014 6.2858e-014 -1.234e-016 -1.234e-016 v ǁVelocityǁ 0.00046418 0.88709 0.049865 0.049865 v Pressure -1.0023 1.0059 -1.9718e-015 -1.3769e-015 v TempK 295.98 303.15 297.81 297.81 v Density 1 1 1 1 v CourantNb 0.47453 8 7.3127 7.3127 v FourierNb 0.17425 10 1.3149 1.3149 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38215 21.346 2.8394 2.8394 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.01 303.15 297.83 297.82 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.65357 17.791 8.6276 8.6276 INSTANT 0.401000000E+02 TIME STEP NUMBER 401 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.42552E-03 0.37685E-01 Friction velocity uk : 0.42552E-03 0.37685E-01 Dimensionless distance yplus : 0.14533E+00 0.12870E+02 Friction thermal sca. tstar : -0.35350E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.10318E+00 0.91378E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.68828E-04 111 0.24393E+00 0.31032E-02 0.78272E+00 c Velocity[X] 0.57838E-03 c Velocity[Y] 0.25248E-02 c Velocity[Z] 0.45843E-29 c Pressure 0.31705E-03 10 0.12692E-07 0.28735E-01 0.10731E-02 c TempK 0.26720E+02 90 0.28218E-03 0.52246E-02 0.18393E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18569 0.18515 -4.055e-007 -4.055e-007 v Velocity[Y] -0.26565 1.011 0.010466 0.010466 v Velocity[Z] -5.6928e-014 5.9819e-014 -1.1241e-016 -1.1241e-016 v ǁVelocityǁ 0.00029551 1.0138 0.050426 0.050426 v Pressure -1.002 1.0079 -2.931e-016 2.1684e-016 v TempK 295.98 303.24 297.83 297.83 v Density 1 1 1 1 v CourantNb 0.35301 8 7.2477 7.2477 v FourierNb 0.1793 10 1.3242 1.3242 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.42037 21.346 2.8598 2.8598 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.98 303.15 297.84 297.84 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85101 17.857 8.5719 8.5719 INSTANT 0.402000000E+02 TIME STEP NUMBER 402 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.39348E-03 0.43046E-01 Friction velocity uk : 0.39348E-03 0.43046E-01 Dimensionless distance yplus : 0.13438E+00 0.14702E+02 Friction thermal sca. tstar : -0.24227E+01 0.97995E-01 Rough dim-less th. sca. tplus : 0.95410E-01 0.10438E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74034E-04 111 0.25893E+00 0.36342E-02 0.88930E+00 c Velocity[X] 0.60992E-03 c Velocity[Y] 0.30243E-02 c Velocity[Z] 0.49204E-29 c Pressure 0.31043E-03 11 0.12063E-07 0.28338E-01 0.12071E-02 c TempK 0.26712E+02 90 0.26924E-03 0.48138E-02 0.18269E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16211 0.17295 -1.2076e-005 -1.2076e-005 v Velocity[Y] -0.31524 0.79053 0.010195 0.010195 v Velocity[Z] -5.4391e-014 5.8465e-014 -1.4097e-016 -1.4097e-016 v ǁVelocityǁ 0.00017651 0.79089 0.050093 0.050093 v Pressure -1.0019 1.0067 -6.0396e-016 0 v TempK 296 303.32 297.85 297.85 v Density 1 1 1 1 v CourantNb 0.33619 8 7.353 7.353 v FourierNb 0.17506 10 1.32 1.32 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41174 21.346 2.8508 2.8508 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 295.98 303.24 297.86 297.86 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.57417 17.828 8.673 8.673 INSTANT 0.403000000E+02 TIME STEP NUMBER 403 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.84617E-03 0.44232E-01 Friction velocity uk : 0.84617E-03 0.44232E-01 Dimensionless distance yplus : 0.28899E+00 0.15106E+02 Friction thermal sca. tstar : -0.24071E+01 0.26360E+00 Rough dim-less th. sca. tplus : 0.20518E+00 0.10725E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71920E-04 111 0.27340E+00 0.31503E-02 0.79796E+00 c Velocity[X] 0.52799E-03 c Velocity[Y] 0.26223E-02 c Velocity[Z] 0.49582E-29 c Pressure 0.30189E-03 10 0.11965E-07 0.27563E-01 0.99808E-03 c TempK 0.26612E+02 89 0.29122E-03 0.40535E-02 0.16293E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18689 0.16065 6.1948e-006 6.1948e-006 v Velocity[Y] -0.21237 0.8479 0.010338 0.010338 v Velocity[Z] -5.5221e-014 6.9173e-014 -1.4864e-016 -1.4864e-016 v ǁVelocityǁ 0.00017131 0.84866 0.049833 0.049833 v Pressure -1.0015 1.0064 -1.3856e-015 -8.4568e-016 v TempK 296.03 303.38 297.87 297.87 v Density 1 1 1 1 v CourantNb 0.42627 8 7.342 7.342 v FourierNb 0.17562 10 1.3187 1.3187 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.4279 21.346 2.8484 2.8484 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296 303.32 297.88 297.87 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.74081 17.642 8.6608 8.6608 INSTANT 0.404000000E+02 TIME STEP NUMBER 404 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.49401E-03 0.42023E-01 Friction velocity uk : 0.49401E-03 0.42023E-01 Dimensionless distance yplus : 0.16872E+00 0.14352E+02 Friction thermal sca. tstar : -0.60149E+01 0.87065E+00 Rough dim-less th. sca. tplus : 0.11979E+00 0.10190E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72900E-04 110 0.26346E+00 0.31746E-02 0.80036E+00 c Velocity[X] 0.55103E-03 c Velocity[Y] 0.26235E-02 c Velocity[Z] 0.48690E-29 c Pressure 0.32263E-03 9 0.13205E-07 0.29541E-01 0.99708E-03 c TempK 0.26540E+02 89 0.25850E-03 0.43393E-02 0.17609E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16584 0.16886 -1.3167e-005 -1.3167e-005 v Velocity[Y] -0.25329 0.82384 0.01036 0.01036 v Velocity[Z] -6.0119e-014 6.4096e-014 -1.1368e-016 -1.1368e-016 v ǁVelocityǁ 0.000303 0.82388 0.05041 0.05041 v Pressure -1.001 1.0062 -2.256e-015 -1.713e-015 v TempK 296.06 303.39 297.88 297.88 v Density 1 1 1 1 v CourantNb 0.29172 8 7.3229 7.3229 v FourierNb 0.17402 10 1.326 1.326 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39023 21.346 2.8643 2.8643 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.03 303.38 297.9 297.89 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.63522 16.786 8.649 8.649 INSTANT 0.405000000E+02 TIME STEP NUMBER 405 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.78181E-03 0.40949E-01 Friction velocity uk : 0.78181E-03 0.40949E-01 Dimensionless distance yplus : 0.26701E+00 0.13985E+02 Friction thermal sca. tstar : -0.52145E+01 0.26288E+00 Rough dim-less th. sca. tplus : 0.18957E+00 0.99294E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72344E-04 118 0.26410E+00 0.33657E-02 0.83490E+00 c Velocity[X] 0.57479E-03 c Velocity[Y] 0.27910E-02 c Velocity[Z] 0.49463E-29 c Pressure 0.30846E-03 10 0.12667E-07 0.27779E-01 0.11011E-02 c TempK 0.26671E+02 88 0.27082E-03 0.43906E-02 0.17918E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.21824 0.16738 1.9532e-005 1.9532e-005 v Velocity[Y] -0.21469 0.7967 0.010341 0.010341 v Velocity[Z] -6.4305e-014 6.445e-014 -1.0156e-016 -1.0156e-016 v ǁVelocityǁ 0.00015998 0.79706 0.050341 0.050341 v Pressure -1.0005 1.0068 -2.1316e-016 3.6863e-016 v TempK 296.05 303.43 297.89 297.89 v Density 1 1 1 1 v CourantNb 0.47657 8 7.3734 7.3734 v FourierNb 0.17774 10 1.3317 1.3317 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39177 21.346 2.8756 2.8756 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.06 303.39 297.91 297.9 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.83887 17.266 8.7051 8.7051 INSTANT 0.406000000E+02 TIME STEP NUMBER 406 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28060E-03 0.41928E-01 Friction velocity uk : 0.28060E-03 0.41928E-01 Dimensionless distance yplus : 0.95833E-01 0.14320E+02 Friction thermal sca. tstar : -0.90733E+01 0.58129E+00 Rough dim-less th. sca. tplus : 0.68040E-01 0.10167E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72475E-04 111 0.26244E+00 0.32377E-02 0.82752E+00 c Velocity[X] 0.54130E-03 c Velocity[Y] 0.26964E-02 c Velocity[Z] 0.51152E-29 c Pressure 0.30639E-03 10 0.13732E-07 0.27951E-01 0.11787E-02 c TempK 0.26755E+02 89 0.25015E-03 0.40888E-02 0.17013E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1738 0.16493 -6.7777e-006 -6.7777e-006 v Velocity[Y] -0.25581 1.0249 0.010406 0.010406 v Velocity[Z] -6.4318e-014 6.3426e-014 -1.2816e-016 -1.2816e-016 v ǁVelocityǁ 8.01e-005 1.0253 0.04998 0.04998 v Pressure -1.0004 1.006 3.5527e-016 8.5652e-016 v TempK 296.03 303.44 297.91 297.91 v Density 1 1 1 1 v CourantNb 0.19029 8 7.3631 7.3631 v FourierNb 0.16536 10 1.3337 1.3337 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38224 21.346 2.8796 2.8796 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.05 303.43 297.92 297.92 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.94756 17.529 8.6967 8.6967 INSTANT 0.407000000E+02 TIME STEP NUMBER 407 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.73565E-03 0.43493E-01 Friction velocity uk : 0.73565E-03 0.43493E-01 Dimensionless distance yplus : 0.25125E+00 0.14854E+02 Friction thermal sca. tstar : -0.10950E+02 0.46072E+00 Rough dim-less th. sca. tplus : 0.17838E+00 0.10546E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70418E-04 111 0.26001E+00 0.30351E-02 0.77063E+00 c Velocity[X] 0.54809E-03 c Velocity[Y] 0.24871E-02 c Velocity[Z] 0.46922E-29 c Pressure 0.32460E-03 10 0.13002E-07 0.29953E-01 0.11621E-02 c TempK 0.26549E+02 88 0.31466E-03 0.38850E-02 0.16298E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19084 0.16923 7.6576e-006 7.6576e-006 v Velocity[Y] -0.19978 0.99582 0.010564 0.010564 v Velocity[Z] -6.0466e-014 7.4204e-014 -1.4486e-016 -1.4486e-016 v ǁVelocityǁ 0.00033929 0.9982 0.049945 0.049945 v Pressure -1.0001 1.007 5.4179e-016 1.0517e-015 v TempK 296.02 303.51 297.92 297.92 v Density 1 1 1 1 v CourantNb 0.21216 8 7.334 7.334 v FourierNb 0.18189 10 1.3413 1.3413 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.42046 21.346 2.8967 2.8967 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.03 303.44 297.94 297.93 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.58367 16.715 8.6753 8.6753 INSTANT 0.408000000E+02 TIME STEP NUMBER 408 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.20284E-03 0.44002E-01 Friction velocity uk : 0.20284E-03 0.44002E-01 Dimensionless distance yplus : 0.69274E-01 0.15028E+02 Friction thermal sca. tstar : -0.11265E+02 0.48056E+00 Rough dim-less th. sca. tplus : 0.49184E-01 0.10670E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70763E-04 110 0.24525E+00 0.31613E-02 0.79481E+00 c Velocity[X] 0.59740E-03 c Velocity[Y] 0.25639E-02 c Velocity[Z] 0.48879E-29 c Pressure 0.32826E-03 11 0.13307E-07 0.29692E-01 0.11116E-02 c TempK 0.26485E+02 88 0.24653E-03 0.32563E-02 0.14972E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17291 0.18596 -4.2056e-006 -4.2056e-006 v Velocity[Y] -0.21979 0.89585 0.010468 0.010468 v Velocity[Z] -5.6505e-014 6.9148e-014 -1.276e-016 -1.276e-016 v ǁVelocityǁ 0.0003889 0.89982 0.04983 0.04983 v Pressure -1 1.0066 -5.5955e-016 -4.3368e-017 v TempK 296.04 303.48 297.93 297.93 v Density 1 1 1 1 v CourantNb 0.21235 8 7.2955 7.2955 v FourierNb 0.1604 10 1.3585 1.3585 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38515 21.346 2.9347 2.9347 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.02 303.51 297.95 297.94 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.79703 16.993 8.654 8.654 INSTANT 0.409000000E+02 TIME STEP NUMBER 409 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.70755E-03 0.42212E-01 Friction velocity uk : 0.70755E-03 0.42212E-01 Dimensionless distance yplus : 0.24165E+00 0.14417E+02 Friction thermal sca. tstar : -0.25967E+01 0.32066E+00 Rough dim-less th. sca. tplus : 0.17157E+00 0.10235E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71076E-04 111 0.27454E+00 0.31588E-02 0.79365E+00 c Velocity[X] 0.56861E-03 c Velocity[Y] 0.25902E-02 c Velocity[Z] 0.47905E-29 c Pressure 0.30325E-03 10 0.14150E-07 0.27294E-01 0.10999E-02 c TempK 0.26423E+02 88 0.35556E-03 0.35333E-02 0.15857E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15056 0.15864 3.3256e-006 3.3256e-006 v Velocity[Y] -0.18787 1.038 0.010506 0.010506 v Velocity[Z] -5.5851e-014 7.0967e-014 -1.1739e-016 -1.1739e-016 v ǁVelocityǁ 0.00032653 1.0381 0.049766 0.049766 v Pressure -0.9999 1.0062 -1.6875e-016 4.0115e-016 v TempK 296.08 303.57 297.94 297.94 v Density 1 1 1 1 v CourantNb 0.16824 8 7.3119 7.3119 v FourierNb 0.16782 10 1.3717 1.3717 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3632 21.346 2.9643 2.9643 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.04 303.48 297.96 297.95 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.63666 17.983 8.6836 8.6836 INSTANT 0.410000000E+02 TIME STEP NUMBER 410 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.41648E-03 0.43651E-01 Friction velocity uk : 0.41648E-03 0.43651E-01 Dimensionless distance yplus : 0.14224E+00 0.14908E+02 Friction thermal sca. tstar : -0.27360E+01 0.85774E+00 Rough dim-less th. sca. tplus : 0.10099E+00 0.10585E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70518E-04 111 0.25898E+00 0.31548E-02 0.78017E+00 c Velocity[X] 0.55954E-03 c Velocity[Y] 0.25953E-02 c Velocity[Z] 0.45845E-29 c Pressure 0.31937E-03 10 0.12906E-07 0.28556E-01 0.11836E-02 c TempK 0.26300E+02 88 0.29236E-03 0.35546E-02 0.15462E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16872 0.16405 -6.0391e-006 -6.0391e-006 v Velocity[Y] -0.21676 0.89199 0.010692 0.010692 v Velocity[Z] -5.3971e-014 6.4919e-014 -1.2547e-016 -1.2547e-016 v ǁVelocityǁ 0.00034078 0.89206 0.050142 0.050142 v Pressure -0.9998 1.0072 -9.77e-016 -4.4452e-016 v TempK 296.14 303.6 297.95 297.95 v Density 1 1 1 1 v CourantNb 0.2924 8 7.3247 7.3247 v FourierNb 0.16448 10 1.3767 1.3767 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35109 21.346 2.976 2.976 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.08 303.57 297.97 297.97 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0443 17.368 8.7015 8.7015 INSTANT 0.411000000E+02 TIME STEP NUMBER 411 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.46534E-03 0.39488E-01 Friction velocity uk : 0.46534E-03 0.39488E-01 Dimensionless distance yplus : 0.15893E+00 0.13486E+02 Friction thermal sca. tstar : -0.74268E+01 0.41245E+00 Rough dim-less th. sca. tplus : 0.11284E+00 0.95750E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73751E-04 112 0.26233E+00 0.34327E-02 0.84046E+00 c Velocity[X] 0.60341E-03 c Velocity[Y] 0.28293E-02 c Velocity[Z] 0.46422E-29 c Pressure 0.31795E-03 10 0.13049E-07 0.27703E-01 0.11891E-02 c TempK 0.26551E+02 89 0.30209E-03 0.40481E-02 0.16926E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1843 0.21448 1.7145e-005 1.7145e-005 v Velocity[Y] -0.16682 0.92451 0.010454 0.010454 v Velocity[Z] -5.2895e-014 6.3338e-014 -1.2666e-016 -1.2666e-016 v ǁVelocityǁ 0.00050037 0.92791 0.05025 0.05025 v Pressure -0.99972 1.0092 -9.8588e-016 -3.6863e-016 v TempK 296.17 303.68 297.96 297.96 v Density 1 1 1 1 v CourantNb 0.11509 8 7.3285 7.3285 v FourierNb 0.14532 10 1.3829 1.3829 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31019 23.379 2.9891 2.9891 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.14 303.6 297.98 297.97 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.035 17.666 8.7114 8.7114 INSTANT 0.412000000E+02 TIME STEP NUMBER 412 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.38335E-03 0.40244E-01 Friction velocity uk : 0.38335E-03 0.40244E-01 Dimensionless distance yplus : 0.13093E+00 0.13745E+02 Friction thermal sca. tstar : -0.55160E+01 0.11451E+01 Rough dim-less th. sca. tplus : 0.92955E-01 0.97584E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72418E-04 113 0.28323E+00 0.31397E-02 0.79363E+00 c Velocity[X] 0.53016E-03 c Velocity[Y] 0.26095E-02 c Velocity[Z] 0.52107E-29 c Pressure 0.31029E-03 10 0.12234E-07 0.26808E-01 0.12555E-02 c TempK 0.26748E+02 91 0.30109E-03 0.40513E-02 0.17291E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17528 0.17591 -2.2999e-006 -2.2999e-006 v Velocity[Y] -0.26954 0.95396 0.010438 0.010438 v Velocity[Z] -5.9408e-014 5.542e-014 -1.4341e-016 -1.4341e-016 v ǁVelocityǁ 0.00091016 0.95536 0.050179 0.050179 v Pressure -0.99953 1.0077 -1.3323e-015 -7.6978e-016 v TempK 296.18 303.71 297.97 297.97 v Density 1 1 1 1 v CourantNb 0.27664 8 7.348 7.348 v FourierNb 0.15985 10 1.3811 1.3811 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34121 25.717 2.9861 2.9861 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.17 303.68 297.99 297.98 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.50029 17.914 8.7291 8.7291 INSTANT 0.413000000E+02 TIME STEP NUMBER 413 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.46208E-03 0.40941E-01 Friction velocity uk : 0.46208E-03 0.40941E-01 Dimensionless distance yplus : 0.15781E+00 0.13982E+02 Friction thermal sca. tstar : -0.95395E+01 0.50951E+00 Rough dim-less th. sca. tplus : 0.11205E+00 0.99273E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.68884E-04 113 0.26245E+00 0.29964E-02 0.75502E+00 c Velocity[X] 0.49343E-03 c Velocity[Y] 0.25030E-02 c Velocity[Z] 0.48052E-29 c Pressure 0.33547E-03 10 0.14015E-07 0.29159E-01 0.12489E-02 c TempK 0.26619E+02 91 0.35141E-03 0.36990E-02 0.16300E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19677 0.20811 1.5214e-006 1.5214e-006 v Velocity[Y] -0.29457 0.87317 0.010736 0.010736 v Velocity[Z] -6.3019e-014 5.8548e-014 -1.2437e-016 -1.2437e-016 v ǁVelocityǁ 0.00042528 0.88141 0.050904 0.050904 v Pressure -0.99936 1.0064 -1.2879e-015 -7.2642e-016 v TempK 296.15 303.72 297.98 297.98 v Density 1 1 1 1 v CourantNb 0.26432 8 7.36 7.36 v FourierNb 0.17584 10 1.372 1.372 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37533 28.288 2.9663 2.9663 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.18 303.71 298 297.99 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.53095 16.993 8.7319 8.7319 INSTANT 0.414000000E+02 TIME STEP NUMBER 414 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.48327E-03 0.41786E-01 Friction velocity uk : 0.48327E-03 0.41786E-01 Dimensionless distance yplus : 0.16505E+00 0.14271E+02 Friction thermal sca. tstar : -0.30246E+01 0.30502E+01 Rough dim-less th. sca. tplus : 0.11718E+00 0.10132E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73524E-04 115 0.27679E+00 0.32348E-02 0.79010E+00 c Velocity[X] 0.58868E-03 c Velocity[Y] 0.26461E-02 c Velocity[Z] 0.45088E-29 c Pressure 0.32927E-03 10 0.12702E-07 0.27514E-01 0.10925E-02 c TempK 0.26581E+02 89 0.25769E-03 0.40295E-02 0.16600E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17445 0.15175 -1.8012e-005 -1.8012e-005 v Velocity[Y] -0.2005 0.93351 0.010568 0.010568 v Velocity[Z] -6.2182e-014 6.1871e-014 -1.278e-016 -1.278e-016 v ǁVelocityǁ 0.00014971 0.93481 0.051165 0.051165 v Pressure -0.99949 1.0059 -7.4607e-016 -1.8431e-016 v TempK 296.12 303.73 297.99 297.99 v Density 1 1 1 1 v CourantNb 0.28848 8 7.3912 7.3912 v FourierNb 0.17084 10 1.3694 1.3694 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41287 28.461 2.962 2.962 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.15 303.72 298.01 298.01 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67404 17.587 8.7606 8.7606 INSTANT 0.415000000E+02 TIME STEP NUMBER 415 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.18998E-03 0.37723E-01 Friction velocity uk : 0.18998E-03 0.37723E-01 Dimensionless distance yplus : 0.64884E-01 0.12884E+02 Friction thermal sca. tstar : -0.13141E+02 0.55289E+00 Rough dim-less th. sca. tplus : 0.46066E-01 0.91472E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73248E-04 112 0.27566E+00 0.31931E-02 0.79810E+00 c Velocity[X] 0.60078E-03 c Velocity[Y] 0.25923E-02 c Velocity[Z] 0.47208E-29 c Pressure 0.32411E-03 11 0.14033E-07 0.27490E-01 0.11317E-02 c TempK 0.26711E+02 88 0.33043E-03 0.45178E-02 0.19494E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16669 0.17475 -8.9781e-006 -8.9781e-006 v Velocity[Y] -0.2394 1.0113 0.010531 0.010531 v Velocity[Z] -6.2398e-014 6.4216e-014 -9.4367e-017 -9.4367e-017 v ǁVelocityǁ 0.00029589 1.0143 0.050851 0.050851 v Pressure -0.99975 1.0064 -1.0925e-015 -5.2042e-016 v TempK 296.11 303.71 298.01 298.01 v Density 1 1 1 1 v CourantNb 0.23903 8 7.41 7.41 v FourierNb 0.16874 10 1.3606 1.3606 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41188 28.461 2.9434 2.9434 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.12 303.73 298.02 298.02 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.71173 17.897 8.7706 8.7706 INSTANT 0.416000000E+02 TIME STEP NUMBER 416 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.62274E-03 0.42946E-01 Friction velocity uk : 0.62274E-03 0.42946E-01 Dimensionless distance yplus : 0.21269E+00 0.14667E+02 Friction thermal sca. tstar : -0.27118E+01 0.12947E+01 Rough dim-less th. sca. tplus : 0.15100E+00 0.10414E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.69884E-04 113 0.25840E+00 0.29902E-02 0.75276E+00 c Velocity[X] 0.56712E-03 c Velocity[Y] 0.24231E-02 c Velocity[Z] 0.45768E-29 c Pressure 0.34313E-03 10 0.15018E-07 0.30629E-01 0.11345E-02 c TempK 0.26646E+02 87 0.27150E-03 0.38480E-02 0.17604E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15904 0.14433 -2.0949e-005 -2.0949e-005 v Velocity[Y] -0.21279 0.85981 0.010414 0.010414 v Velocity[Z] -6.2867e-014 6.2506e-014 -1.1813e-016 -1.1813e-016 v ǁVelocityǁ 0.00015259 0.86355 0.051037 0.051037 v Pressure -1 1.0074 -1.5099e-016 4.4452e-016 v TempK 296.12 303.69 298.02 298.02 v Density 1 1 1 1 v CourantNb 0.41383 8 7.3788 7.3788 v FourierNb 0.18561 10 1.3483 1.3483 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.44028 21.346 2.9109 2.9109 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.11 303.71 298.04 298.03 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.84434 17.274 8.7271 8.7271 INSTANT 0.417000000E+02 TIME STEP NUMBER 417 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.15436E-03 0.44793E-01 Friction velocity uk : 0.15436E-03 0.44793E-01 Dimensionless distance yplus : 0.52719E-01 0.15298E+02 Friction thermal sca. tstar : -0.32521E+01 0.47742E+00 Rough dim-less th. sca. tplus : 0.37429E-01 0.10861E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.68956E-04 112 0.27175E+00 0.29711E-02 0.73089E+00 c Velocity[X] 0.54309E-03 c Velocity[Y] 0.24280E-02 c Velocity[Z] 0.52647E-29 c Pressure 0.33124E-03 11 0.15226E-07 0.30417E-01 0.11284E-02 c TempK 0.26661E+02 87 0.30993E-03 0.37333E-02 0.17257E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1616 0.16542 -8.8955e-006 -8.8955e-006 v Velocity[Y] -0.21297 1.0118 0.010647 0.010647 v Velocity[Z] -6.692e-014 6.3966e-014 -1.0654e-016 -1.0654e-016 v ǁVelocityǁ 0.00045843 1.0133 0.051604 0.051604 v Pressure -1.0001 1.0057 1.0392e-015 1.7239e-015 v TempK 296.15 303.65 298.02 298.02 v Density 1 1 1 1 v CourantNb 0.12196 8 7.3875 7.3875 v FourierNb 0.18393 10 1.3537 1.3537 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39547 21.346 2.9235 2.9235 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.12 303.69 298.05 298.04 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.65566 17.489 8.7412 8.7412 INSTANT 0.418000000E+02 TIME STEP NUMBER 418 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.57031E-03 0.40257E-01 Friction velocity uk : 0.57031E-03 0.40257E-01 Dimensionless distance yplus : 0.19478E+00 0.13749E+02 Friction thermal sca. tstar : -0.44095E+01 0.77515E+00 Rough dim-less th. sca. tplus : 0.13829E+00 0.97615E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70792E-04 114 0.25845E+00 0.31936E-02 0.75731E+00 c Velocity[X] 0.60106E-03 c Velocity[Y] 0.25925E-02 c Velocity[Z] 0.59822E-29 c Pressure 0.33927E-03 10 0.14724E-07 0.31972E-01 0.12046E-02 c TempK 0.26909E+02 88 0.32445E-03 0.38427E-02 0.17735E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17684 0.18127 -2.1342e-005 -2.1342e-005 v Velocity[Y] -0.20998 0.89817 0.010664 0.010664 v Velocity[Z] -6.2408e-014 6.5801e-014 -1.3207e-016 -1.3207e-016 v ǁVelocityǁ 0.00022687 0.91546 0.051983 0.051983 v Pressure -1.0003 1.0068 -1.128e-015 -5.8547e-016 v TempK 296.16 303.58 298.02 298.02 v Density 1 1 1 1 v CourantNb 0.35344 8 7.449 7.449 v FourierNb 0.18726 10 1.3373 1.3373 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39972 21.346 2.8889 2.8889 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.15 303.65 298.05 298.04 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0429 17.849 8.7863 8.7863 INSTANT 0.419000000E+02 TIME STEP NUMBER 419 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.44201E-03 0.45429E-01 Friction velocity uk : 0.44201E-03 0.45429E-01 Dimensionless distance yplus : 0.15096E+00 0.15515E+02 Friction thermal sca. tstar : -0.26703E+01 0.67694E+00 Rough dim-less th. sca. tplus : 0.10718E+00 0.11016E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73203E-04 111 0.27301E+00 0.34675E-02 0.82377E+00 c Velocity[X] 0.62690E-03 c Velocity[Y] 0.28406E-02 c Velocity[Z] 0.54096E-29 c Pressure 0.34615E-03 11 0.13404E-07 0.33241E-01 0.12148E-02 c TempK 0.27348E+02 85 0.24988E-03 0.31770E-02 0.14828E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17422 0.162 4.0741e-006 4.0741e-006 v Velocity[Y] -0.20981 0.98163 0.010497 0.010497 v Velocity[Z] -6.267e-014 6.5473e-014 -1.0518e-016 -1.0518e-016 v ǁVelocityǁ 0.00015657 0.9872 0.050915 0.050915 v Pressure -1.0004 1.009 -1.0214e-015 -4.0115e-016 v TempK 296.15 303.55 298.03 298.03 v Density 1 1 1 1 v CourantNb 0.30191 8 7.4118 7.4118 v FourierNb 0.15332 10 1.3315 1.3315 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37343 21.346 2.8773 2.8773 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.16 303.58 298.05 298.05 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.87993 17.974 8.7434 8.7434 INSTANT 0.420000000E+02 TIME STEP NUMBER 420 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.47635E-03 0.40419E-01 Friction velocity uk : 0.47635E-03 0.40419E-01 Dimensionless distance yplus : 0.16269E+00 0.13804E+02 Friction thermal sca. tstar : -0.74136E+01 0.44359E+00 Rough dim-less th. sca. tplus : 0.11550E+00 0.98009E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72454E-04 110 0.26547E+00 0.29185E-02 0.71619E+00 c Velocity[X] 0.55849E-03 c Velocity[Y] 0.23600E-02 c Velocity[Z] 0.55183E-29 c Pressure 0.34862E-03 10 0.15599E-07 0.34136E-01 0.13614E-02 c TempK 0.27199E+02 82 0.34922E-03 0.24434E-02 0.13754E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18929 0.17807 -8.8385e-006 -8.8385e-006 v Velocity[Y] -0.2117 0.94324 0.010669 0.010669 v Velocity[Z] -5.2174e-014 6.4437e-014 -1.4898e-016 -1.4898e-016 v ǁVelocityǁ 0.00027996 0.94407 0.051494 0.051494 v Pressure -1.0005 1.0054 3.7303e-016 1.0408e-015 v TempK 296.13 303.43 298.04 298.04 v Density 1 1 1 1 v CourantNb 0.18933 8 7.3323 7.3323 v FourierNb 0.16866 10 1.3234 1.3234 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41078 21.346 2.8595 2.8595 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.15 303.55 298.06 298.06 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.56585 17.6 8.6557 8.6557 INSTANT 0.421000000E+02 TIME STEP NUMBER 421 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32298E-03 0.44371E-01 Friction velocity uk : 0.32298E-03 0.44371E-01 Dimensionless distance yplus : 0.11031E+00 0.15154E+02 Friction thermal sca. tstar : -0.92440E+01 0.64030E+00 Rough dim-less th. sca. tplus : 0.78316E-01 0.10759E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72216E-04 110 0.26379E+00 0.33187E-02 0.79751E+00 c Velocity[X] 0.57683E-03 c Velocity[Y] 0.27419E-02 c Velocity[Z] 0.53383E-29 c Pressure 0.33499E-03 10 0.15955E-07 0.31884E-01 0.11670E-02 c TempK 0.27375E+02 81 0.29391E-03 0.31353E-02 0.15718E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18354 0.17766 -3.4282e-006 -3.4282e-006 v Velocity[Y] -0.2132 0.86494 0.010503 0.010503 v Velocity[Z] -5.573e-014 6.5677e-014 -1.0939e-016 -1.0939e-016 v ǁVelocityǁ 2.3894e-005 0.86791 0.051145 0.051145 v Pressure -1.0003 1.008 7.9936e-017 6.7221e-016 v TempK 296.11 303.44 298.05 298.05 v Density 1 1 1 1 v CourantNb 0.17634 8 7.3145 7.3145 v FourierNb 0.16235 10 1.3267 1.3267 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34655 21.346 2.8669 2.8669 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.13 303.43 298.07 298.06 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.83036 17.862 8.6412 8.6412 INSTANT 0.422000000E+02 TIME STEP NUMBER 422 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.32933E-03 0.46136E-01 Friction velocity uk : 0.32933E-03 0.46136E-01 Dimensionless distance yplus : 0.11248E+00 0.15757E+02 Friction thermal sca. tstar : -0.25621E+02 0.48044E+00 Rough dim-less th. sca. tplus : 0.79856E-01 0.11187E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73274E-04 109 0.26989E+00 0.33507E-02 0.82674E+00 c Velocity[X] 0.54060E-03 c Velocity[Y] 0.28101E-02 c Velocity[Z] 0.61917E-29 c Pressure 0.33591E-03 10 0.17651E-07 0.30974E-01 0.13173E-02 c TempK 0.27515E+02 81 0.28586E-03 0.24706E-02 0.15112E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16911 0.16063 -1.6421e-005 -1.6421e-005 v Velocity[Y] -0.23403 0.99425 0.010612 0.010612 v Velocity[Z] -5.1862e-014 5.8818e-014 -1.4016e-016 -1.4016e-016 v ǁVelocityǁ 6.4035e-005 0.99512 0.050577 0.050577 v Pressure -1.0005 1.0078 -9.4147e-016 -3.5779e-016 v TempK 296.11 303.42 298.05 298.05 v Density 1 1 1 1 v CourantNb 0.40728 8 7.3005 7.3005 v FourierNb 0.11712 10 1.3414 1.3414 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.28943 22.94 2.8998 2.8998 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.11 303.44 298.08 298.07 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75792 17.925 8.6419 8.6419 INSTANT 0.423000000E+02 TIME STEP NUMBER 423 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.33648E-03 0.46289E-01 Friction velocity uk : 0.33648E-03 0.46289E-01 Dimensionless distance yplus : 0.11492E+00 0.15809E+02 Friction thermal sca. tstar : -0.56696E+01 0.36552E+00 Rough dim-less th. sca. tplus : 0.81589E-01 0.11224E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74134E-04 110 0.26756E+00 0.33265E-02 0.79799E+00 c Velocity[X] 0.57531E-03 c Velocity[Y] 0.27512E-02 c Velocity[Z] 0.55763E-29 c Pressure 0.33919E-03 10 0.15018E-07 0.30946E-01 0.12481E-02 c TempK 0.27523E+02 80 0.33180E-03 0.24903E-02 0.14502E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15489 0.18029 1.7132e-005 1.7132e-005 v Velocity[Y] -0.28989 0.98188 0.010602 0.010602 v Velocity[Z] -5.2045e-014 5.6458e-014 -9.3527e-017 -9.3527e-017 v ǁVelocityǁ 0.00027814 0.98196 0.050293 0.050293 v Pressure -1.0011 1.0072 -3.5527e-016 2.9273e-016 v TempK 296.15 303.39 298.06 298.06 v Density 1 1 1 1 v CourantNb 0.26845 8 7.2098 7.2098 v FourierNb 0.12883 10 1.3575 1.3575 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.31837 25.234 2.9362 2.9362 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.11 303.42 298.08 298.08 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.75114 17.251 8.5673 8.5673 INSTANT 0.424000000E+02 TIME STEP NUMBER 424 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28648E-03 0.41137E-01 Friction velocity uk : 0.28648E-03 0.41137E-01 Dimensionless distance yplus : 0.97843E-01 0.14049E+02 Friction thermal sca. tstar : -0.31092E+01 0.36081E+00 Rough dim-less th. sca. tplus : 0.69467E-01 0.99748E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76837E-04 108 0.27074E+00 0.33904E-02 0.82417E+00 c Velocity[X] 0.58453E-03 c Velocity[Y] 0.28059E-02 c Velocity[Z] 0.60883E-29 c Pressure 0.33530E-03 10 0.13713E-07 0.29585E-01 0.12062E-02 c TempK 0.27429E+02 82 0.25082E-03 0.28773E-02 0.15650E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18294 0.2048 1.9777e-006 1.9777e-006 v Velocity[Y] -0.25214 0.84474 0.010435 0.010435 v Velocity[Z] -5.8986e-014 5.5369e-014 -1.4468e-016 -1.4468e-016 v ǁVelocityǁ 0.00010617 0.84566 0.05026 0.05026 v Pressure -1.0011 1.0075 -1.3056e-015 -7.1557e-016 v TempK 296.19 303.34 298.08 298.08 v Density 1 1 1 1 v CourantNb 0.28694 8 7.223 7.223 v FourierNb 0.14171 10 1.3855 1.3855 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35021 27.758 2.9986 2.9986 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.15 303.39 298.09 298.09 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.52706 17.009 8.6085 8.6085 INSTANT 0.425000000E+02 TIME STEP NUMBER 425 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.17483E-03 0.45083E-01 Friction velocity uk : 0.17483E-03 0.45083E-01 Dimensionless distance yplus : 0.59711E-01 0.15397E+02 Friction thermal sca. tstar : -0.25391E+01 0.48210E+00 Rough dim-less th. sca. tplus : 0.42394E-01 0.10932E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72316E-04 112 0.25574E+00 0.31705E-02 0.79379E+00 c Velocity[X] 0.55665E-03 c Velocity[Y] 0.26138E-02 c Velocity[Z] 0.61011E-29 c Pressure 0.32197E-03 10 0.15403E-07 0.28391E-01 0.12305E-02 c TempK 0.27438E+02 82 0.27207E-03 0.25654E-02 0.14289E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16313 0.17232 6.929e-006 6.929e-006 v Velocity[Y] -0.22289 0.88053 0.01055 0.01055 v Velocity[Z] -6.0484e-014 5.8758e-014 -1.6643e-016 -1.6643e-016 v ǁVelocityǁ 0.00041758 0.88874 0.04974 0.04974 v Pressure -1.0005 1.0056 -7.1054e-016 -3.2526e-017 v TempK 296.21 303.35 298.09 298.09 v Density 1 1 1 1 v CourantNb 0.035298 8 7.2255 7.2255 v FourierNb 0.15588 10 1.3938 1.3938 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37471 28.461 3.0188 3.0188 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.19 303.34 298.11 298.1 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.6778 17.973 8.6193 8.6193 INSTANT 0.426000000E+02 TIME STEP NUMBER 426 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.33120E-03 0.43761E-01 Friction velocity uk : 0.33120E-03 0.43761E-01 Dimensionless distance yplus : 0.11312E+00 0.14946E+02 Friction thermal sca. tstar : -0.54564E+01 0.45515E+00 Rough dim-less th. sca. tplus : 0.80310E-01 0.10611E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73851E-04 109 0.26736E+00 0.32478E-02 0.79162E+00 c Velocity[X] 0.55635E-03 c Velocity[Y] 0.26914E-02 c Velocity[Z] 0.55319E-29 c Pressure 0.32868E-03 11 0.16407E-07 0.28288E-01 0.12056E-02 c TempK 0.27374E+02 84 0.28658E-03 0.27894E-02 0.14884E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14473 0.20939 -1.3489e-005 -1.3489e-005 v Velocity[Y] -0.28222 0.93898 0.010778 0.010778 v Velocity[Z] -6.784e-014 5.8081e-014 -1.4393e-016 -1.4393e-016 v ǁVelocityǁ 7.8692e-005 0.94211 0.049747 0.049747 v Pressure -0.99994 1.0071 -1.7764e-016 4.0115e-016 v TempK 296.2 303.32 298.1 298.1 v Density 1 1 1 1 v CourantNb 0.2032 8 7.2135 7.2135 v FourierNb 0.17147 10 1.4049 1.4049 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38906 28.461 3.0433 3.0433 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.21 303.35 298.12 298.11 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72055 17.607 8.6184 8.6184 INSTANT 0.427000000E+02 TIME STEP NUMBER 427 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.90034E-03 0.42575E-01 Friction velocity uk : 0.90034E-03 0.42575E-01 Dimensionless distance yplus : 0.30749E+00 0.14541E+02 Friction thermal sca. tstar : -0.28443E+01 0.62828E+00 Rough dim-less th. sca. tplus : 0.21831E+00 0.10324E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76804E-04 110 0.28593E+00 0.35690E-02 0.83878E+00 c Velocity[X] 0.59514E-03 c Velocity[Y] 0.29739E-02 c Velocity[Z] 0.54641E-29 c Pressure 0.32075E-03 11 0.14373E-07 0.28130E-01 0.12707E-02 c TempK 0.27362E+02 85 0.25429E-03 0.36252E-02 0.16540E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17046 0.17297 -5.168e-006 -5.168e-006 v Velocity[Y] -0.26329 0.87426 0.010678 0.010678 v Velocity[Z] -7.1889e-014 6.6629e-014 -1.113e-016 -1.113e-016 v ǁVelocityǁ 7.2379e-005 0.88084 0.050327 0.050327 v Pressure -1.0001 1.0061 -4.3521e-016 8.6736e-017 v TempK 296.17 303.24 298.12 298.12 v Density 1 1 1 1 v CourantNb 0.20302 8 7.1898 7.1898 v FourierNb 0.17426 10 1.4284 1.4284 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38092 28.461 3.0952 3.0952 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.2 303.32 298.13 298.13 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.79129 17.598 8.6183 8.6183 INSTANT 0.428000000E+02 TIME STEP NUMBER 428 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.28848E-03 0.42729E-01 Friction velocity uk : 0.28848E-03 0.42729E-01 Dimensionless distance yplus : 0.98525E-01 0.14593E+02 Friction thermal sca. tstar : -0.83743E+01 0.17465E+00 Rough dim-less th. sca. tplus : 0.69951E-01 0.10361E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76573E-04 109 0.29000E+00 0.34724E-02 0.84161E+00 c Velocity[X] 0.59291E-03 c Velocity[Y] 0.28795E-02 c Velocity[Z] 0.55807E-29 c Pressure 0.32100E-03 10 0.13566E-07 0.27960E-01 0.12410E-02 c TempK 0.27581E+02 85 0.26916E-03 0.30904E-02 0.14672E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16275 0.19772 -1.7905e-005 -1.7905e-005 v Velocity[Y] -0.29306 0.95292 0.010487 0.010487 v Velocity[Z] -7.2808e-014 6.4624e-014 -1.4898e-016 -1.4898e-016 v ǁVelocityǁ 0.00035526 0.95314 0.049796 0.049796 v Pressure -1.0002 1.0076 -2.1227e-015 -1.5721e-015 v TempK 296.15 303.19 298.14 298.14 v Density 1 1 1 1 v CourantNb 0.17225 8 7.2122 7.2122 v FourierNb 0.16787 10 1.4295 1.4295 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.36425 28.461 3.0984 3.0984 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.17 303.24 298.15 298.15 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.87921 17.93 8.6417 8.6417 INSTANT 0.429000000E+02 TIME STEP NUMBER 429 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26767E-03 0.44233E-01 Friction velocity uk : 0.26767E-03 0.44233E-01 Dimensionless distance yplus : 0.91416E-01 0.15107E+02 Friction thermal sca. tstar : -0.12547E+02 0.50005E-01 Rough dim-less th. sca. tplus : 0.64904E-01 0.10726E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.76157E-04 109 0.28056E+00 0.33760E-02 0.83461E+00 c Velocity[X] 0.58547E-03 c Velocity[Y] 0.27906E-02 c Velocity[Z] 0.55335E-29 c Pressure 0.33750E-03 10 0.14079E-07 0.29561E-01 0.13211E-02 c TempK 0.27565E+02 85 0.30045E-03 0.36343E-02 0.15430E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.174 0.17084 2.2808e-005 2.2808e-005 v Velocity[Y] -0.24711 0.92858 0.010437 0.010437 v Velocity[Z] -6.7231e-014 6.8959e-014 -1.2859e-016 -1.2859e-016 v ǁVelocityǁ 0.00025198 0.93198 0.049749 0.049749 v Pressure -1.0002 1.0062 -4.5297e-016 1.6263e-016 v TempK 296.17 303.18 298.16 298.16 v Density 1 1 1 1 v CourantNb 0.41091 8 7.2078 7.2078 v FourierNb 0.13929 10 1.4302 1.4302 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.29733 27.928 3.1018 3.1018 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.15 303.19 298.17 298.17 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.94807 17.772 8.638 8.638 INSTANT 0.430000000E+02 TIME STEP NUMBER 430 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.62382E-03 0.39969E-01 Friction velocity uk : 0.62382E-03 0.39969E-01 Dimensionless distance yplus : 0.21305E+00 0.13651E+02 Friction thermal sca. tstar : -0.61133E+01 0.54892E-01 Rough dim-less th. sca. tplus : 0.15126E+00 0.96917E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73016E-04 109 0.25689E+00 0.32293E-02 0.79644E+00 c Velocity[X] 0.60086E-03 c Velocity[Y] 0.26284E-02 c Velocity[Z] 0.61314E-29 c Pressure 0.32572E-03 10 0.11529E-07 0.28465E-01 0.12072E-02 c TempK 0.27440E+02 84 0.28374E-03 0.39705E-02 0.18308E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.20467 0.21801 -5.7542e-006 -5.7542e-006 v Velocity[Y] -0.29904 0.83436 0.010474 0.010474 v Velocity[Z] -6.0594e-014 5.9449e-014 -1.4546e-016 -1.4546e-016 v ǁVelocityǁ 0.00017527 0.83481 0.049791 0.049791 v Pressure -1.0009 1.0065 -6.3061e-016 -2.1684e-017 v TempK 296.22 303.16 298.17 298.17 v Density 1 1 1 1 v CourantNb 0.23067 8 7.1283 7.1283 v FourierNb 0.15322 10 1.4384 1.4384 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.32707 28.461 3.1203 3.1203 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.17 303.18 298.19 298.18 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.92249 17.826 8.5667 8.5667 INSTANT 0.431000000E+02 TIME STEP NUMBER 431 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26097E-03 0.44547E-01 Friction velocity uk : 0.26097E-03 0.44547E-01 Dimensionless distance yplus : 0.89131E-01 0.15214E+02 Friction thermal sca. tstar : -0.42933E+01 0.23299E+00 Rough dim-less th. sca. tplus : 0.63281E-01 0.10802E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.80459E-04 110 0.27558E+00 0.34703E-02 0.85032E+00 c Velocity[X] 0.60672E-03 c Velocity[Y] 0.28635E-02 c Velocity[Z] 0.56196E-29 c Pressure 0.31385E-03 9 0.14266E-07 0.26462E-01 0.12761E-02 c TempK 0.27472E+02 83 0.29444E-03 0.38608E-02 0.17243E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15784 0.16051 5.0267e-006 5.0267e-006 v Velocity[Y] -0.21433 1.0702 0.010237 0.010237 v Velocity[Z] -6.5031e-014 6.902e-014 -9.8397e-017 -9.8397e-017 v ǁVelocityǁ 0.00013886 1.0713 0.04953 0.04953 v Pressure -1.0014 1.0067 -8.8818e-017 4.8789e-016 v TempK 296.27 303.12 298.18 298.18 v Density 1 1 1 1 v CourantNb 0.26283 8 7.1214 7.1214 v FourierNb 0.16855 10 1.4457 1.4457 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35977 26.662 3.133 3.133 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.22 303.16 298.2 298.19 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.77196 17.956 8.5671 8.5671 INSTANT 0.432000000E+02 TIME STEP NUMBER 432 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.16271E-03 0.42706E-01 Friction velocity uk : 0.16271E-03 0.42706E-01 Dimensionless distance yplus : 0.55570E-01 0.14585E+02 Friction thermal sca. tstar : -0.22211E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.39453E-01 0.10355E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.77578E-04 108 0.28020E+00 0.31848E-02 0.80772E+00 c Velocity[X] 0.51801E-03 c Velocity[Y] 0.26668E-02 c Velocity[Z] 0.51135E-29 c Pressure 0.31346E-03 10 0.13124E-07 0.27275E-01 0.12236E-02 c TempK 0.27492E+02 85 0.30470E-03 0.33702E-02 0.15383E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14448 0.18775 -1.1932e-006 -1.1932e-006 v Velocity[Y] -0.20595 0.86943 0.010449 0.010449 v Velocity[Z] -6.2936e-014 7.4342e-014 -1.4816e-016 -1.4816e-016 v ǁVelocityǁ 0.00039947 0.86978 0.049973 0.049973 v Pressure -1.0017 1.0057 -7.1942e-016 -1.0842e-016 v TempK 296.29 303.11 298.2 298.2 v Density 1 1 1 1 v CourantNb 0.177 8 7.155 7.155 v FourierNb 0.14309 10 1.4465 1.4465 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.3719 28.461 3.1319 3.1319 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.27 303.15 298.21 298.21 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.41373 17.567 8.6015 8.6015 INSTANT 0.433000000E+02 TIME STEP NUMBER 433 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.76245E-03 0.47301E-01 Friction velocity uk : 0.76245E-03 0.47301E-01 Dimensionless distance yplus : 0.26040E+00 0.16155E+02 Friction thermal sca. tstar : -0.69881E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.18488E+00 0.11469E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72794E-04 109 0.25211E+00 0.31769E-02 0.77774E+00 c Velocity[X] 0.58044E-03 c Velocity[Y] 0.25964E-02 c Velocity[Z] 0.48427E-29 c Pressure 0.32752E-03 10 0.12265E-07 0.28471E-01 0.11547E-02 c TempK 0.27540E+02 85 0.32836E-03 0.43755E-02 0.16532E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23416 0.17211 9.3069e-006 9.3069e-006 v Velocity[Y] -0.188 0.8862 0.010403 0.010403 v Velocity[Z] -6.1248e-014 7.5292e-014 -1.2512e-016 -1.2512e-016 v ǁVelocityǁ 0.00051947 0.88754 0.050623 0.050623 v Pressure -1.0021 1.0066 -2.256e-015 -1.6914e-015 v TempK 296.29 303.08 298.21 298.21 v Density 1 1 1 1 v CourantNb 0.28403 8 7.2135 7.2135 v FourierNb 0.1574 10 1.4375 1.4375 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40909 25.558 3.1135 3.1135 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.29 303.15 298.23 298.22 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.59099 17.908 8.6511 8.6511 INSTANT 0.434000000E+02 TIME STEP NUMBER 434 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.14905E-03 0.40504E-01 Friction velocity uk : 0.14905E-03 0.40504E-01 Dimensionless distance yplus : 0.50903E-01 0.13833E+02 Friction thermal sca. tstar : -0.29231E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.36141E-01 0.98215E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74869E-04 109 0.26966E+00 0.35470E-02 0.85760E+00 c Velocity[X] 0.59546E-03 c Velocity[Y] 0.29515E-02 c Velocity[Z] 0.60355E-29 c Pressure 0.30993E-03 10 0.10615E-07 0.27076E-01 0.11515E-02 c TempK 0.27770E+02 86 0.25883E-03 0.45005E-02 0.16497E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16591 0.16729 -1.7343e-005 -1.7343e-005 v Velocity[Y] -0.33551 0.89396 0.010211 0.010211 v Velocity[Z] -6.332e-014 6.6048e-014 -1.4204e-016 -1.4204e-016 v ǁVelocityǁ 0.00032355 0.89536 0.05006 0.05006 v Pressure -1.0024 1.0076 -3.4639e-016 2.1684e-016 v TempK 296.28 303 298.23 298.23 v Density 1 1 1 1 v CourantNb 0.32402 8 7.2908 7.2908 v FourierNb 0.17314 10 1.4293 1.4293 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37445 28.114 3.0958 3.0958 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.29 303.15 298.24 298.24 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.9993 17.979 8.7201 8.7201 INSTANT 0.435000000E+02 TIME STEP NUMBER 435 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.83906E-03 0.43939E-01 Friction velocity uk : 0.83906E-03 0.43939E-01 Dimensionless distance yplus : 0.28656E+00 0.15007E+02 Friction thermal sca. tstar : -0.55001E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.20345E+00 0.10654E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75771E-04 108 0.26442E+00 0.33030E-02 0.81407E+00 c Velocity[X] 0.55772E-03 c Velocity[Y] 0.27453E-02 c Velocity[Z] 0.57715E-29 c Pressure 0.31037E-03 10 0.11757E-07 0.26737E-01 0.11825E-02 c TempK 0.27754E+02 87 0.24804E-03 0.41888E-02 0.16222E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23072 0.17818 4.401e-006 4.401e-006 v Velocity[Y] -0.23948 0.87285 0.010321 0.010321 v Velocity[Z] -6.5441e-014 7.3305e-014 -1.2299e-016 -1.2299e-016 v ǁVelocityǁ 6.1891e-005 0.87287 0.050332 0.050332 v Pressure -1.0022 1.0072 -9.1482e-016 -3.0358e-016 v TempK 296.29 303.01 298.25 298.25 v Density 1 1 1 1 v CourantNb 0.22907 8 7.2403 7.2403 v FourierNb 0.15457 10 1.4424 1.4424 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39319 28.461 3.1248 3.1248 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.28 303.15 298.26 298.25 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.6466 17.767 8.6828 8.6828 INSTANT 0.436000000E+02 TIME STEP NUMBER 436 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.82827E-03 0.40659E-01 Friction velocity uk : 0.82827E-03 0.40659E-01 Dimensionless distance yplus : 0.28288E+00 0.13886E+02 Friction thermal sca. tstar : -0.39629E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.20084E+00 0.98591E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75981E-04 108 0.23164E+00 0.33054E-02 0.81331E+00 c Velocity[X] 0.58336E-03 c Velocity[Y] 0.27220E-02 c Velocity[Z] 0.51131E-29 c Pressure 0.32362E-03 10 0.11123E-07 0.27750E-01 0.11164E-02 c TempK 0.27879E+02 87 0.31416E-03 0.41548E-02 0.16869E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17669 0.16612 -4.2777e-006 -4.2777e-006 v Velocity[Y] -0.23364 0.87377 0.010389 0.010389 v Velocity[Z] -7.1305e-014 6.3982e-014 -1.4487e-016 -1.4487e-016 v ǁVelocityǁ 0.00024688 0.8764 0.050686 0.050686 v Pressure -1.0013 1.0066 -3.7303e-016 3.2526e-016 v TempK 296.33 303 298.27 298.27 v Density 1 1 1 1 v CourantNb 0.095549 8 7.2852 7.2852 v FourierNb 0.16509 10 1.4385 1.4385 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.35239 28.461 3.1169 3.1169 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.29 303.15 298.28 298.27 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.94314 17.63 8.7237 8.7237 INSTANT 0.437000000E+02 TIME STEP NUMBER 437 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.40273E-03 0.44745E-01 Friction velocity uk : 0.40273E-03 0.44745E-01 Dimensionless distance yplus : 0.13754E+00 0.15282E+02 Friction thermal sca. tstar : -0.12488E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.97653E-01 0.10850E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74828E-04 109 0.25024E+00 0.33081E-02 0.82718E+00 c Velocity[X] 0.58474E-03 c Velocity[Y] 0.27233E-02 c Velocity[Z] 0.57726E-29 c Pressure 0.31588E-03 9 0.14612E-07 0.28102E-01 0.11674E-02 c TempK 0.27982E+02 88 0.28400E-03 0.43180E-02 0.17038E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19684 0.16881 2.8365e-007 2.8365e-007 v Velocity[Y] -0.2728 0.82922 0.010208 0.010208 v Velocity[Z] -7.1656e-014 6.9527e-014 -1.238e-016 -1.238e-016 v ǁVelocityǁ 0.00016215 0.82925 0.050555 0.050555 v Pressure -1.0002 1.0078 -9.5035e-016 -3.7947e-016 v TempK 296.39 302.99 298.28 298.28 v Density 1 1 1 1 v CourantNb 0.2542 8 7.3195 7.3195 v FourierNb 0.17528 10 1.4296 1.4296 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37414 21.699 3.0968 3.0968 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.33 303.15 298.29 298.29 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.92558 17.449 8.7492 8.7492 INSTANT 0.438000000E+02 TIME STEP NUMBER 438 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26698E-03 0.40478E-01 Friction velocity uk : 0.26698E-03 0.40478E-01 Dimensionless distance yplus : 0.91182E-01 0.13824E+02 Friction thermal sca. tstar : -0.31376E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.64738E-01 0.98151E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72849E-04 112 0.24895E+00 0.31564E-02 0.79192E+00 c Velocity[X] 0.54510E-03 c Velocity[Y] 0.26113E-02 c Velocity[Z] 0.57545E-29 c Pressure 0.30707E-03 10 0.12955E-07 0.26061E-01 0.10571E-02 c TempK 0.27906E+02 90 0.25386E-03 0.45582E-02 0.17735E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.1674 0.16656 -1.1839e-005 -1.1839e-005 v Velocity[Y] -0.25055 0.84687 0.010296 0.010296 v Velocity[Z] -6.1445e-014 6.3101e-014 -1.2681e-016 -1.2681e-016 v ǁVelocityǁ 0.00020297 0.84827 0.050068 0.050068 v Pressure -0.99961 1.0063 -2.6645e-016 3.6863e-016 v TempK 296.45 303 298.28 298.28 v Density 1 1 1 1 v CourantNb 0.41197 8 7.2925 7.2925 v FourierNb 0.17596 10 1.4427 1.4427 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.41155 23.869 3.1245 3.1245 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.39 303.15 298.31 298.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.67404 16.889 8.7353 8.7353 INSTANT 0.439000000E+02 TIME STEP NUMBER 439 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.10448E-02 0.43866E-01 Friction velocity uk : 0.10448E-02 0.43866E-01 Dimensionless distance yplus : 0.35684E+00 0.14982E+02 Friction thermal sca. tstar : -0.29533E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.25335E+00 0.10637E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72937E-04 111 0.25148E+00 0.31487E-02 0.78236E+00 c Velocity[X] 0.58072E-03 c Velocity[Y] 0.25680E-02 c Velocity[Z] 0.49253E-29 c Pressure 0.32878E-03 10 0.11820E-07 0.26697E-01 0.10743E-02 c TempK 0.27762E+02 91 0.30291E-03 0.54962E-02 0.17979E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.19057 0.19086 8.0269e-007 8.0269e-007 v Velocity[Y] -0.23433 0.78825 0.010304 0.010304 v Velocity[Z] -6.0702e-014 6.3069e-014 -1.3183e-016 -1.3183e-016 v ǁVelocityǁ 0.00051882 0.78994 0.050947 0.050947 v Pressure -0.99954 1.0069 6.6613e-016 1.2251e-015 v TempK 296.48 303 298.28 298.28 v Density 1 1 1 1 v CourantNb 0.34616 8 7.2013 7.2013 v FourierNb 0.18098 10 1.4636 1.4636 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38641 23.904 3.1683 3.1683 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.45 303.15 298.31 298.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.85378 17.987 8.6649 8.6649 INSTANT 0.440000000E+02 TIME STEP NUMBER 440 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.71674E-03 0.39699E-01 Friction velocity uk : 0.71674E-03 0.39699E-01 Dimensionless distance yplus : 0.24479E+00 0.13558E+02 Friction thermal sca. tstar : -0.30527E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.17380E+00 0.96263E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74859E-04 116 0.26131E+00 0.32689E-02 0.80585E+00 c Velocity[X] 0.57446E-03 c Velocity[Y] 0.26944E-02 c Velocity[Z] 0.55288E-29 c Pressure 0.30424E-03 10 0.11669E-07 0.24210E-01 0.11010E-02 c TempK 0.27818E+02 93 0.26714E-03 0.58297E-02 0.17744E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18858 0.16624 -8.0236e-006 -8.0236e-006 v Velocity[Y] -0.22636 0.87564 0.01031 0.01031 v Velocity[Z] -6.7818e-014 6.217e-014 -1.1006e-016 -1.1006e-016 v ǁVelocityǁ 0.00020389 0.87707 0.050863 0.050863 v Pressure -0.99938 1.0062 -1.7764e-016 3.4694e-016 v TempK 296.48 303.07 298.28 298.28 v Density 1 1 1 1 v CourantNb 0.46264 8 7.3189 7.3189 v FourierNb 0.18288 10 1.4784 1.4784 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39782 26.294 3.2004 3.2004 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.48 303.15 298.31 298.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.9723 17.488 8.7974 8.7974 INSTANT 0.441000000E+02 TIME STEP NUMBER 441 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.53511E-03 0.43263E-01 Friction velocity uk : 0.53511E-03 0.43263E-01 Dimensionless distance yplus : 0.18276E+00 0.14776E+02 Friction thermal sca. tstar : -0.10366E+02 0.00000E+00 Rough dim-less th. sca. tplus : 0.12975E+00 0.10491E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.70465E-04 112 0.26570E+00 0.31636E-02 0.77134E+00 c Velocity[X] 0.52302E-03 c Velocity[Y] 0.26405E-02 c Velocity[Z] 0.53500E-29 c Pressure 0.30824E-03 13 0.11986E-07 0.25260E-01 0.10474E-02 c TempK 0.27652E+02 91 0.31041E-03 0.55860E-02 0.17735E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16174 0.17095 5.0469e-006 5.0469e-006 v Velocity[Y] -0.20767 1.0398 0.010524 0.010524 v Velocity[Z] -6.0813e-014 6.077e-014 -1.284e-016 -1.284e-016 v ǁVelocityǁ 0.00021661 1.044 0.051314 0.051314 v Pressure -0.99947 1.0074 -6.0396e-016 4.3368e-017 v TempK 296.47 303.15 298.28 298.28 v Density 1 1 1 1 v CourantNb 0.17037 8 7.3023 7.3023 v FourierNb 0.17815 10 1.4738 1.4738 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38028 25.454 3.1889 3.1889 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.48 303.15 298.31 298.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.47268 17.589 8.7761 8.7761 INSTANT 0.442000000E+02 TIME STEP NUMBER 442 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.26852E-03 0.40501E-01 Friction velocity uk : 0.26852E-03 0.40501E-01 Dimensionless distance yplus : 0.91706E-01 0.13832E+02 Friction thermal sca. tstar : -0.75940E+01 0.00000E+00 Rough dim-less th. sca. tplus : 0.65110E-01 0.98208E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74311E-04 112 0.26140E+00 0.35994E-02 0.83768E+00 c Velocity[X] 0.58880E-03 c Velocity[Y] 0.30106E-02 c Velocity[Z] 0.49803E-29 c Pressure 0.31425E-03 10 0.11417E-07 0.25969E-01 0.10788E-02 c TempK 0.27656E+02 90 0.25924E-03 0.52884E-02 0.17636E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.17776 0.207 -1.0583e-005 -1.0583e-005 v Velocity[Y] -0.24065 0.84121 0.010449 0.010449 v Velocity[Z] -6.1366e-014 5.5849e-014 -1.2082e-016 -1.2082e-016 v ǁVelocityǁ 0.00014458 0.84397 0.051798 0.051798 v Pressure -0.99971 1.0077 -8.8818e-018 6.9389e-016 v TempK 296.47 303.21 298.29 298.29 v Density 1 1 1 1 v CourantNb 0.1865 8 7.3134 7.3134 v FourierNb 0.17512 10 1.4662 1.4662 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.39086 22.097 3.174 3.174 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.47 303.15 298.31 298.3 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.42744 17.97 8.7796 8.7796 INSTANT 0.443000000E+02 TIME STEP NUMBER 443 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.12097E-03 0.43256E-01 Friction velocity uk : 0.12097E-03 0.43256E-01 Dimensionless distance yplus : 0.41316E-01 0.14773E+02 Friction thermal sca. tstar : -0.43084E+01 0.46904E+00 Rough dim-less th. sca. tplus : 0.29334E-01 0.10489E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.75003E-04 112 0.26307E+00 0.35671E-02 0.83912E+00 c Velocity[X] 0.59527E-03 c Velocity[Y] 0.29718E-02 c Velocity[Z] 0.55247E-29 c Pressure 0.30424E-03 10 0.11704E-07 0.26517E-01 0.11333E-02 c TempK 0.27733E+02 90 0.29293E-03 0.52947E-02 0.17908E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.23577 0.14611 1.0434e-005 1.0434e-005 v Velocity[Y] -0.26042 0.97021 0.010309 0.010309 v Velocity[Z] -6.0679e-014 5.5434e-014 -1.5056e-016 -1.5056e-016 v ǁVelocityǁ 0.00023297 0.97365 0.051826 0.051826 v Pressure -0.99979 1.0066 1.5099e-016 7.481e-016 v TempK 296.48 303.29 298.29 298.29 v Density 1 1 1 1 v CourantNb 0.40771 8 7.3955 7.3955 v FourierNb 0.16614 10 1.4454 1.4454 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.40323 22.604 3.1308 3.1308 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.47 303.21 298.32 298.31 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.72026 17.797 8.841 8.841 INSTANT 0.444000000E+02 TIME STEP NUMBER 444 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.53820E-03 0.40106E-01 Friction velocity uk : 0.53820E-03 0.40106E-01 Dimensionless distance yplus : 0.18381E+00 0.13698E+02 Friction thermal sca. tstar : -0.35905E+01 0.36181E+00 Rough dim-less th. sca. tplus : 0.13050E+00 0.97250E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.72660E-04 111 0.25017E+00 0.35933E-02 0.85530E+00 c Velocity[X] 0.56439E-03 c Velocity[Y] 0.30289E-02 c Velocity[Z] 0.51269E-29 c Pressure 0.30909E-03 10 0.11320E-07 0.26356E-01 0.11819E-02 c TempK 0.27811E+02 90 0.24075E-03 0.53004E-02 0.18713E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16084 0.18271 7.1629e-007 7.1629e-007 v Velocity[Y] -0.26283 0.88646 0.01042 0.01042 v Velocity[Z] -5.3331e-014 5.6314e-014 -1.29e-016 -1.29e-016 v ǁVelocityǁ 0.00019314 0.8865 0.0519 0.0519 v Pressure -0.99969 1.0079 3.9968e-016 9.3241e-016 v TempK 296.51 303.44 298.3 298.3 v Density 1 1 1 1 v CourantNb 0.41777 8 7.3666 7.3666 v FourierNb 0.16122 10 1.4336 1.4336 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.34414 24.864 3.1047 3.1047 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.48 303.29 298.32 298.32 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.81024 17.595 8.8002 8.8002 INSTANT 0.445000000E+02 TIME STEP NUMBER 445 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.30060E-03 0.43811E-01 Friction velocity uk : 0.30060E-03 0.43811E-01 Dimensionless distance yplus : 0.10267E+00 0.14963E+02 Friction thermal sca. tstar : -0.71452E+01 0.49906E+00 Rough dim-less th. sca. tplus : 0.72891E-01 0.10623E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.74566E-04 111 0.26190E+00 0.33559E-02 0.83895E+00 c Velocity[X] 0.56746E-03 c Velocity[Y] 0.27884E-02 c Velocity[Z] 0.47409E-29 c Pressure 0.31752E-03 14 0.13424E-07 0.26924E-01 0.11646E-02 c TempK 0.27723E+02 91 0.25802E-03 0.50495E-02 0.19419E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.18164 0.1711 9.3589e-006 9.3589e-006 v Velocity[Y] -0.25721 0.8853 0.010242 0.010242 v Velocity[Z] -5.1553e-014 5.6859e-014 -1.3656e-016 -1.3656e-016 v ǁVelocityǁ 0.00026021 0.88553 0.05116 0.05116 v Pressure -0.99965 1.007 -1.5099e-015 -9.4326e-016 v TempK 296.53 303.52 298.31 298.31 v Density 1 1 1 1 v CourantNb 0.14186 8 7.3754 7.3754 v FourierNb 0.16009 10 1.4281 1.4281 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37855 27.351 3.0905 3.0905 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.51 303.44 298.33 298.32 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.41987 17.942 8.8035 8.8035 INSTANT 0.446000000E+02 TIME STEP NUMBER 446 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.65037E-03 0.42977E-01 Friction velocity uk : 0.65037E-03 0.42977E-01 Dimensionless distance yplus : 0.22212E+00 0.14678E+02 Friction thermal sca. tstar : -0.36152E+01 0.45437E+00 Rough dim-less th. sca. tplus : 0.15770E+00 0.10421E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71372E-04 111 0.25097E+00 0.32278E-02 0.80111E+00 c Velocity[X] 0.59138E-03 c Velocity[Y] 0.26365E-02 c Velocity[Z] 0.45632E-29 c Pressure 0.31797E-03 10 0.14710E-07 0.25942E-01 0.10497E-02 c TempK 0.27384E+02 91 0.30497E-03 0.49031E-02 0.18596E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16933 0.24402 -7.1066e-006 -7.1066e-006 v Velocity[Y] -0.24461 0.78036 0.010233 0.010233 v Velocity[Z] -5.7005e-014 5.7608e-014 -1.1555e-016 -1.1555e-016 v ǁVelocityǁ 0.00012092 0.78098 0.05176 0.05176 v Pressure -0.9992 1.0061 -1.7764e-016 4.6621e-016 v TempK 296.53 303.52 298.32 298.32 v Density 1 1 1 1 v CourantNb 0.015817 8 7.2832 7.2832 v FourierNb 0.1761 10 1.447 1.447 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38133 21.346 3.1312 3.1312 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.53 303.52 298.34 298.33 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.71673 17.489 8.7302 8.7302 INSTANT 0.447000000E+02 TIME STEP NUMBER 447 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.11231E-02 0.39524E-01 Friction velocity uk : 0.11231E-02 0.39524E-01 Dimensionless distance yplus : 0.38356E+00 0.13499E+02 Friction thermal sca. tstar : -0.38488E+01 0.67017E+00 Rough dim-less th. sca. tplus : 0.27232E+00 0.95839E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.73443E-04 112 0.25848E+00 0.34256E-02 0.83729E+00 c Velocity[X] 0.63200E-03 c Velocity[Y] 0.27936E-02 c Velocity[Z] 0.46008E-29 c Pressure 0.30987E-03 10 0.12131E-07 0.24814E-01 0.10856E-02 c TempK 0.27379E+02 92 0.30789E-03 0.44117E-02 0.17210E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15367 0.17448 3.141e-006 3.141e-006 v Velocity[Y] -0.22225 0.90064 0.010127 0.010127 v Velocity[Z] -6.3376e-014 5.8215e-014 -1.4019e-016 -1.4019e-016 v ǁVelocityǁ 0.00014322 0.90093 0.052033 0.052033 v Pressure -0.99913 1.0062 -7.1942e-016 -1.5179e-016 v TempK 296.53 303.51 298.33 298.33 v Density 1 1 1 1 v CourantNb 0.2499 8 7.4237 7.4237 v FourierNb 0.17741 10 1.4379 1.4379 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.37906 21.346 3.1084 3.1084 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.53 303.52 298.35 298.35 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.91621 17.737 8.8617 8.8617 INSTANT 0.448000000E+02 TIME STEP NUMBER 448 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.91588E-03 0.41115E-01 Friction velocity uk : 0.91588E-03 0.41115E-01 Dimensionless distance yplus : 0.31280E+00 0.14042E+02 Friction thermal sca. tstar : -0.32946E+01 0.14625E+01 Rough dim-less th. sca. tplus : 0.22208E+00 0.99697E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 448, Physical time 0.44800E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: 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 0.72660E-04 113 0.24365E+00 0.32960E-02 0.81034E+00 c Velocity[X] 0.58743E-03 c Velocity[Y] 0.27086E-02 c Velocity[Z] 0.51943E-29 c Pressure 0.29650E-03 10 0.12657E-07 0.23871E-01 0.11232E-02 c TempK 0.27511E+02 90 0.30850E-03 0.40370E-02 0.16727E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.15617 0.16775 2.932e-006 2.932e-006 v Velocity[Y] -0.21334 0.83948 0.010335 0.010335 v Velocity[Z] -6.8072e-014 5.839e-014 -1.4369e-016 -1.4369e-016 v ǁVelocityǁ 0.00014238 0.8406 0.051949 0.051949 v Pressure -0.99929 1.0066 -6.9278e-016 -7.5894e-017 v TempK 296.53 303.56 298.34 298.34 v Density 1 1 1 1 v CourantNb 0.28946 8 7.4648 7.4648 v FourierNb 0.1791 10 1.4279 1.4279 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38231 21.346 3.0881 3.0881 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.53 303.51 298.36 298.36 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.65881 17.303 8.8928 8.8928 INSTANT 0.449000000E+02 TIME STEP NUMBER 449 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.55624E-03 0.41990E-01 Friction velocity uk : 0.55624E-03 0.41990E-01 Dimensionless distance yplus : 0.18997E+00 0.14341E+02 Friction thermal sca. tstar : -0.62368E+01 0.63840E+00 Rough dim-less th. sca. tplus : 0.13488E+00 0.10182E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.71426E-04 114 0.24891E+00 0.32893E-02 0.80835E+00 c Velocity[X] 0.57640E-03 c Velocity[Y] 0.27129E-02 c Velocity[Z] 0.46130E-29 c Pressure 0.30652E-03 10 0.11775E-07 0.25014E-01 0.11180E-02 c TempK 0.27594E+02 88 0.32621E-03 0.40157E-02 0.16230E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.16581 0.17452 1.597e-005 1.597e-005 v Velocity[Y] -0.21495 0.81307 0.010318 0.010318 v Velocity[Z] -6.8335e-014 5.7853e-014 -1.4877e-016 -1.4877e-016 v ǁVelocityǁ 0.0001806 0.81342 0.051912 0.051912 v Pressure -0.99952 1.0067 -6.839e-016 -3.2526e-017 v TempK 296.53 303.58 298.35 298.35 v Density 1 1 1 1 v CourantNb 0.42523 8 7.4744 7.4744 v FourierNb 0.16796 10 1.4169 1.4169 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.38512 21.346 3.0653 3.0653 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.53 303.56 298.37 298.37 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.70528 17.969 8.8913 8.8913 INSTANT 0.450000000E+02 TIME STEP NUMBER 450 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 320 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 12800 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 : 0.72133E-03 0.41923E-01 Friction velocity uk : 0.72133E-03 0.41923E-01 Dimensionless distance yplus : 0.24636E+00 0.14318E+02 Friction thermal sca. tstar : -0.73106E+01 0.54152E+00 Rough dim-less th. sca. tplus : 0.17491E+00 0.10166E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 320 Total number of wall faces : 320 ------------------------------------------------------------ Write final restart files checkpoint at iteration 450, Physical time 0.45000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint: 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 0.71346E-04 113 0.25279E+00 0.33510E-02 0.82015E+00 c Velocity[X] 0.56813E-03 c Velocity[Y] 0.27828E-02 c Velocity[Z] 0.47687E-29 c Pressure 0.30141E-03 10 0.12607E-07 0.25104E-01 0.11193E-02 c TempK 0.27651E+02 87 0.28628E-03 0.34593E-02 0.15865E-03 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a TempK a Local Time Step ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - --------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.14658 0.21161 7.7105e-006 7.7105e-006 v Velocity[Y] -0.30019 0.77392 0.010325 0.010325 v Velocity[Z] -6.8558e-014 5.6911e-014 -1.3678e-016 -1.3678e-016 v ǁVelocityǁ 0.00033284 0.77458 0.052077 0.052077 v Pressure -0.99983 1.0076 -1.5365e-015 -8.3484e-016 v TempK 296.56 303.55 298.36 298.36 v Density 1 1 1 1 v CourantNb 0.16525 8 7.4583 7.4583 v FourierNb 0.18475 10 1.41 1.41 v total_pressure 1.0131e+005 1.0132e+005 1.0132e+005 1.0132e+005 v Local Time Step 0.42363 22.07 3.0519 3.0519 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v TempK 296.53 303.58 298.38 298.38 v Boundary Density 1 1 1 1 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.68001 17.866 8.8682 8.8682 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation